Author Topic: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion  (Read 89585 times)

Online gongora

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Discussion thread for Starlink v1.0 Flight 7.

Check the Starlink Index Thread for links to more Starlink information.

NSF Threads for Starlink v1.0 Flight 7: Discussion / Updates

NSF News Articles for Starlink:
https://www.nasaspaceflight.com/?s=Starlink

June 3, 2020 at approximately 9:25pm EDT (01:25 UTC on June 4) on Falcon 9 (booster 1049.5) from SLC-40.  ASDS landing on the newly remodeled JRTI is expected.  Targeting deployment orbit of 190x380km.

Payload: A batch of 60 Starlink satellites.  At least one should be a "VisorSat" with the new sunshade to help reduce the brightness of the satellites as seen from the ground.

Please use the Starlink Discussion Thread for all general discussion on Starlink.

L2 SpaceX:
https://forum.nasaspaceflight.com/index.php?board=60.0

From a previous mission's Press Kit:
Quote
Each Starlink satellite weights approximately 260 kg and features a compact, flat-panel design that minimizes volume, allowing for a dense launch stack to take full advantage of Falcon 9’s launch capabilities. With four powerful phased array and two parabolic antennas on each satellite ... At end of their life cycle, the satellites will utilize their on-board propulsion system to deorbit over the course of a few months. In the unlikely event their propulsion system becomes inoperable, the satellites will burn up in Earth’s atmosphere within 1-5 years, significantly less than the hundreds or thousands of years required at higher altitudes. Further, Starlink components are designed for full demisability.

Starlink is targeting service in the Northern U.S. and Canada in 2020, rapidly expanding to near global coverage of the populated world by 2021. Additional information on the system can be found at starlink.com.
« Last Edit: 06/04/2020 08:28 pm by input~2 »

Offline scr00chy

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET May 2020
« Reply #1 on: 04/23/2020 11:04 am »
Quote
The next SpaceX Falcon 9 rocket from Cape Canaveral will launch the next batch of 60 Starlink
satellites from pad 40 on early May TBA
http://www.launchphotography.com/Delta_4_Atlas_5_Falcon_9_Launch_Viewing.html

Offline Elthiryel

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET May 2020
« Reply #2 on: 04/25/2020 12:27 pm »
Booster 1049 is going to be used for the fifth time during this flight.

Source: https://nextspaceflight.com/launches/details/2572

Previous missions:
Telstar 18 VANTAGE - September 2018
Iridium-8 - January 2019
Starlink-1 (V0.9) - May 2019
Starlink-3 (V1.0 L2) - January 2020
GO for launch, GO for age of reflight

Offline PM3

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET May 2020
« Reply #3 on: 04/27/2020 07:39 pm »
May 7, 11:30 UTC (7:30 am EDT)

https://spaceflightnow.com/launch-schedule/
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Online gongora

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET May 2020
« Reply #4 on: 04/27/2020 07:44 pm »
https://twitter.com/jeff_foust/status/1254818901944344576
Quote
Elon Musk is giving a presentation at a public meeting of an Astro2020 astrophysics decadal survey cmte meeting on efforts to mitigate brightness of Starlink satellites. First “VisorSat” satellites, with sunshade to block reflections off antennas, planned to be on next launch.

https://twitter.com/CatHofacker/status/1254821075176886285
Quote
Elon Musk giving a short presentation at a meeting for the Astro 2020 decadal, says we'll have a "VisorSat" on the next Starlink launch that has a sunshade to reduce the satellites' brightness.

Offline Mammutti

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 7, 2020
« Reply #5 on: 04/28/2020 07:29 pm »
Quote
ATLANTIC OCEAN - FLORIDA - CAPE CANAVERAL: EASTERN RANGE OP# X0056 STARLINK V1.0-L7

Eastern range will be conducting hazardous operations surface to unlimited within portions of Warning Areas W497A, W497B, W137F/G, W138E,
W139E/F, W140E, W122 and the following Hazard Areas.
From 2836 55.22N 8036 0.35W
TO 2848N 8024W
TO 2854N 8017W
TO 2917N 7949W
TO 2915N 7946W
TO 2841N 8017W
TO 2834N 8025W
TO 2831N 8031W
TO 2830 25.65N 8033 0.42W to beginning
From 3158N 7658W
TO 3309N 7558W
TO 3323N 7536W
TO 3323N 7456W
TO 3315N 7437W
TO 3248N 7435W
TO 3229N 7459W
TO 3140N 7642W to beginning
Hazard periods for primary launch day and backup launch days;
Primary launch day: 07 / 1110Z thru 07 / 1237Z May 20. Preferred T-0 is 1115Z.
Backup launch day (1): 08 / 1050Z thru 08 / 1217Z May 20. Preferred T-0 is 1055Z.
Backup launch day (2): 09 / 1023Z thru 09 / 1210Z May 20. Preferred T-0 is 1023Z.
Backup launch day (3): 10 / 1001Z thru 10 / 1148Z May 20. Preferred T-0 is 1001Z.
Backup launch day (4): 11 / 0940Z thru 11 / 1127Z May 20. Preferred T-0 is 0940Z.
Backup launch day (5): 12 / 0918Z thru 12 / 1105Z May 20. Preferred T-0 is 0918Z.
Backup launch day (6): 13 / 0856Z thru 13 / 1043Z May 20. Preferred T-0 is 0856Z

https://www.navcen.uscg.gov/pdf/lnms/lnm07172020.pdf

Offline paul2k19

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 7, 2020
« Reply #6 on: 05/01/2020 12:59 pm »
Apparently launch has been delayed (nextspaceflight)

Offline Elthiryel

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 7, 2020
« Reply #7 on: 05/01/2020 02:02 pm »
Ben Cooper has also changed the date from "May 7" to "May TBA", so that confirms the delay.
GO for launch, GO for age of reflight

Offline PM3

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May, 2020
« Reply #8 on: 05/04/2020 05:58 pm »
May 18
07:09-08:09 UTC (3:09-4:09 a.m. EDT)

https://spaceflightnow.com/launch-schedule/
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Offline jketch

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May, 2020
« Reply #9 on: 05/04/2020 11:41 pm »
I'm surprised this is launching so close to DM-2 given that both are ASDS landings. There are only nine days to return the Starlink 8 booster to port, unload it, and get to the DM-2 booster landing site.

Offline Nevyn72

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May, 2020
« Reply #10 on: 05/04/2020 11:44 pm »
I'm surprised this is launching so close to DM-2 given that both are ASDS landings. There are only nine days to return the Starlink 8 booster to port, unload it, and get to the DM-2 booster landing site.

If only they had a second ASDS available*......  ;)

* Will JRTI be ready by then?

Offline AndrewRG10

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May, 2020
« Reply #11 on: 05/04/2020 11:57 pm »
I'm surprised this is launching so close to DM-2 given that both are ASDS landings. There are only nine days to return the Starlink 8 booster to port, unload it, and get to the DM-2 booster landing site.
Nusantara Satu and DM-1 were just 8 days apart, they managed to do it but it was a very quick turn around from booster unloading to departure. They should be able to do a 9 day turnaround and a delay of 3 days should help them. But it would be a lot more helpful to have JRTI used this mission.
« Last Edit: 05/04/2020 11:58 pm by AndrewRG10 »

Offline atsf90east

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May, 2020
« Reply #12 on: 05/05/2020 01:42 am »
I'm surprised this is launching so close to DM-2 given that both are ASDS landings. There are only nine days to return the Starlink 8 booster to port, unload it, and get to the DM-2 booster landing site.

If only they had a second ASDS available*......  ;)

* Will JRTI be ready by then?

A Starlink booster recovery would be the perfect post-retrofit shakedown
Attended Launches: Space Shuttle: STS-85, STS-95, STS-96, STS-103. Falcon 9: Thaicom-8

Offline wannamoonbase

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May, 2020
« Reply #13 on: 05/05/2020 01:59 am »
I'm surprised this is launching so close to DM-2 given that both are ASDS landings. There are only nine days to return the Starlink 8 booster to port, unload it, and get to the DM-2 booster landing site.

If only they had a second ASDS available*......  ;)

* Will JRTI be ready by then?

A Starlink booster recovery would be the perfect post-retrofit shakedown

Yeah, lets see what tricks they are installing on JRTI.

I have a theory, based on no information, that they are developing Super ASDS information to prepare for Super Heavy down range recovery.
Starship, Vulcan and Ariane 6 have all reached orbit.  New Glenn, well we are waiting!

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May, 2020
« Reply #14 on: 05/05/2020 02:56 am »
I'm surprised this is launching so close to DM-2 given that both are ASDS landings. There are only nine days to return the Starlink 8 booster to port, unload it, and get to the DM-2 booster landing site.

If only they had a second ASDS available*......  ;)

* Will JRTI be ready by then?

A Starlink booster recovery would be the perfect post-retrofit shakedown

Yeah, lets see what tricks they are installing on JRTI.

I have a theory, based on no information, that they are developing Super ASDS information to prepare for Super Heavy down range recovery.

This is starting to wander a bit too far from the thread topic.

Offline Raul

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May, 2020
« Reply #15 on: 05/05/2020 06:14 am »
According Stage2 Debris Reentry NOTAM in Mazatlan Oceanic area it looks to be NET May 17.
Quote
MAZATLAN OCEANIC FIR
NOTAM #: A2521/20      Class: International      Start Date UTC: 05/17/2020 0857      End Date UTC: 05/19/2020 0920      Status: Active
A2521/20 NOTAMN
Q) MMFO/QRDCA/IV/BO/W/000/999/
A) MMFO
B) 2005170857
C) 2005190920
D) 0857/1003 DAY 17 MAY
   0836/0942 DAY 18 MAY
   0814/0920 DAY 19 MAY
E) DANGEROUS AREA FOR REENTRY OF ROCKET FALCON-9
   LATERAL LIMIT: AREA FORMED BY THE UNION OF THE FOLLOWING POINTS:
                  05 00 00N  120 00 00W
                  11 24 43N  120 00 00W
                  16 19 00N  114 48 00W
                  15 16 00N  113 01 00W
                  07 44 00N  116 14 00W
                  05 50 17N  117 24 06W
                  05 00 00N  120 00 00W
F) GND
G) UNL

Offline Elthiryel

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET May 17, 2020
« Reply #16 on: 05/07/2020 11:59 am »
According to the Spaceflight Now Launch Schedule, the launch is NET May 17 (which confirms information inferred from the NOTAM), approximately 08:00 UTC.

They also added a comment:
Quote
Updated to clarify the possibility of launching May 17, assuming range availability.

Atlas V 501 is slated to launch on May 16 (precise launch time unknown) with OTV-6 mission, which may affect range availability.

Ben Cooper has also adjusted launch time on his website.

http://www.launchphotography.com/Delta_4_Atlas_5_Falcon_9_Launch_Viewing.html
Quote
May 17 at the very earliest, around 3:30-4am EDT
« Last Edit: 05/07/2020 05:00 pm by Elthiryel »
GO for launch, GO for age of reflight

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET May 17, 2020
« Reply #17 on: 05/07/2020 06:47 pm »
Re: Eastern Range support May 16/May 17

They can support CC/KSC launches separated by less than 24 hours.  How much less, I don't know.

Falcon launches (from CC/KSC only?) no longer require range radar support for range safety.  Velocity (speed and direction) is computed, and compared to the computed trajectory, on board the LV via GPS.

Seeking clarification and/or correction.  Confirmation would be nice, too. :)
« Last Edit: 05/07/2020 06:50 pm by zubenelgenubi »
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Offline Hummy

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 18, 2020
« Reply #18 on: 05/08/2020 09:00 pm »
Next launch satellites are going to be the first to start rolling during orbit raising to reduce visibility.

Offline The Roadie

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 18, 2020
« Reply #19 on: 05/08/2020 10:41 pm »
Next launch satellites are going to be the first to start rolling during orbit raising to reduce visibility.
Source?
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Offline allins

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 18, 2020
« Reply #20 on: 05/08/2020 11:39 pm »
Next launch satellites are going to be the first to start rolling during orbit raising to reduce visibility.
Source?
The graphic above (Under the Launch 7 title)

Offline The Roadie

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 18, 2020
« Reply #21 on: 05/08/2020 11:42 pm »
Next launch satellites are going to be the first to start rolling during orbit raising to reduce visibility.
Source?
The graphic above (Under the Launch 7 title)
I can read the slide. Where did the SLIDE come from. Assume a SpaceX presentation, but sources need to be attributed here.
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« Last Edit: 05/09/2020 12:33 am by gongora »

Offline Elthiryel

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 18, 2020
« Reply #23 on: 05/09/2020 01:06 am »
Source: https://www.spacex.com/news/2020/04/28/starlink-update
Quote
The first unit is flying on the next launch, and by flight 9 in June all future Starlink satellites will have sun visors.
Quote
As previously noted, the first VisorSat prototype will launch in May and we will have these black, specular visors on all satellites by June.
GO for launch, GO for age of reflight

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 18, 2020
« Reply #24 on: 05/11/2020 07:18 pm »
When is the static fire going to happen? I think they don't want it to happen with the Atlas right next to it, especially as it has the payload on top. So it has to be quite a few days before for the launch to happen the day after OTV-6

Offline scr00chy

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET May 17, 2020
« Reply #25 on: 05/13/2020 12:15 pm »
I spy a vertical Falcon 9 with a fairing full of Starlink satellites. Static fire may occur this morning. We are heading into a busy ops period with two launches getting ready at CCAFS.  #SpaceX

https://twitter.com/julia_bergeron/status/1260533688351195136

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Offline edkyle99

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET May 17, 2020
« Reply #27 on: 05/13/2020 02:39 pm »
When is the static fire going to happen? I think they don't want it to happen with the Atlas right next to it, especially as it has the payload on top. So it has to be quite a few days before for the launch to happen the day after OTV-6
SLC 40 and 41 are 1.5 miles (2.4 km) apart.  They were spaced that far apart for a reason. 

 - Ed Kyle

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #28 on: 05/13/2020 04:19 pm »
twitter.com/spacex/status/1260603520102748161

Quote
Static fire test of Falcon 9 complete—targeting Sunday, May 17 at 3:53 a.m. EDT, 7:53 UTC, for launch of the eighth Starlink mission, which will lift off from SLC-40 in Florida

https://twitter.com/spacex/status/1260603521402986496

Quote
The first stage rocket booster supporting this mission previously  launched two Starlink missions, as well as the Iridium-8 and Telstar 18 VANTAGE missions

So 1049.5   8)
« Last Edit: 05/13/2020 04:23 pm by FutureSpaceTourist »

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #29 on: 05/13/2020 07:37 pm »
https://twitter.com/eg0911/status/1260628535015813121

Quote
OCISLY on its way out of Port Canaveral for the upcoming starlink launch. @SpaceXFleet

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET May 17, 2020
« Reply #30 on: 05/14/2020 12:15 am »
When is the static fire going to happen? I think they don't want it to happen with the Atlas right next to it, especially as it has the payload on top. So it has to be quite a few days before for the launch to happen the day after OTV-6
SLC 40 and 41 are 1.5 miles (2.4 km) apart.  They were spaced that far apart for a reason. 

 - Ed Kyle

And, Atlas was in its VIF at the time of the Falcon Static Fire.
From Back-to-back launches scheduled from Cape Canaveral this weekend, dated May 8
Quote
ULA ground crews plan to transfer the Atlas 5 rocket to pad 41 Thursday morning [May 14] from the Vertical Integration Facility, where the launcher was stacked over the last few weeks. ULA installed the X-37B spacecraft on top of the Atlas 5 inside the vertical hangar May 5.
« Last Edit: 05/14/2020 12:17 am by zubenelgenubi »
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET May 17, 2020
« Reply #31 on: 05/14/2020 06:42 am »
When is the static fire going to happen? I think they don't want it to happen with the Atlas right next to it, especially as it has the payload on top. So it has to be quite a few days before for the launch to happen the day after OTV-6
SLC 40 and 41 are 1.5 miles (2.4 km) apart.  They were spaced that far apart for a reason. 

 - Ed Kyle

If I remember correctly, when AMOS-6 exploded some debris reached pad 41, but as the Atlas was still in the VIF, no damage to the vehicle was reported. I doubt ULA would want to have their rocket on the pad when another one is a potential danger next door.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #32 on: 05/14/2020 02:34 pm »
Weather 80 % favorable on launch day, 90 % on backup day.
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #33 on: 05/14/2020 02:44 pm »
Not looking too good for booster recovery ops; wonder if they'll postpone or take the chance.
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #34 on: 05/14/2020 02:49 pm »
Back-to-back launches scheduled from Cape Canaveral this weekend, dated May 13
Quote
The Falcon 9 launch attempt Sunday will only go ahead if the Atlas 5 rocket takes off as scheduled Saturday, according to Brig. Gen. Doug Schiess, commander of the 45th Space Wing, which manages range operations at Cape Canaveral Air Force Station.

For now, the Atlas 5 has Sunday booked as a backup launch opportunity on the Eastern Range at Cape Canaveral.
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #35 on: 05/14/2020 02:49 pm »
Not looking too good for booster recovery ops; wonder if they'll postpone or take the chance.

Depending on the weather for the Atlas launch, the choice may be made for them anyway.
« Last Edit: 05/14/2020 02:49 pm by gongora »

Offline wannamoonbase

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #36 on: 05/14/2020 07:58 pm »
Has it been mentioned if this payload fairing is new or being reused?
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #37 on: 05/14/2020 09:28 pm »
https://twitter.com/spacexfleet/status/1261039191913369601

Quote
Fleet Update!

OCISLY progress to LZ:
█████░░░░░░░ 42%

Ms. Tree and Ms. Chief are still docked at Port Canaveral at this time.

Offline Elthiryel

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #38 on: 05/15/2020 12:47 am »
And now the fairing catchers are also out of the port.

https://twitter.com/spacecoast_stve/status/1261088099410546690?s=21

Has it been mentioned if this payload fairing is new or being reused?
The last time when they were reusing the fairings, they mentioned it in one of the post static fire tweets, it did not happen this time, so I think we can assume these are the new fairings.
GO for launch, GO for age of reflight

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #39 on: 05/15/2020 01:11 am »
The last time when they were reusing the fairings, they mentioned it in one of the post static fire tweets, it did not happen this time, so I think we can assume these are the new fairings.

The definitive answer will be in the press kit, typically released the day before launch.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #40 on: 05/15/2020 02:31 am »
https://twitter.com/TSKelso/status/1261116678802309121

Quote
CelesTrak just received state vectors from @SpaceX for the next #Starlink launch, set for May 17 at 0753 UTC. We have generated SupTLEs (assuming it will be launch 2020-030). Those are now available at https://celestrak.com/NORAD/elements/supplemental/. I will update if anything changes.
« Last Edit: 05/15/2020 02:31 am by gongora »

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #41 on: 05/15/2020 11:36 am »
It would be nice if this weekend didn't get blown up by weather.  :P
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #42 on: 05/15/2020 02:11 pm »
L-2 launch forecast still 80% GO (but tomorrow’s ULA launch still only 40%)
« Last Edit: 05/15/2020 02:12 pm by FutureSpaceTourist »

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #43 on: 05/15/2020 03:57 pm »
Re: weather at the Cape and down-range at OCISLY:
It may be better for all concerned if the launch cadence is Sunday-Atlas V//Monday-Falcon 9.
« Last Edit: 05/16/2020 02:50 pm by zubenelgenubi »
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #44 on: 05/15/2020 04:00 pm »
Will SpaceX be able to do the nine-day turnaround if Starlink goes off on Monday? Like, how fast can OCISLY return B1049 before going back out again for DM-2?
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #45 on: 05/15/2020 04:08 pm »
Will SpaceX be able to do the nine-day turnaround if Starlink goes off on Monday? Like, how fast can OCISLY return B1049 before going back out again for DM-2?

Maybe we will see JRTI back in action soon.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #46 on: 05/15/2020 04:27 pm »
Will SpaceX be able to do the nine-day turnaround if Starlink goes off on Monday? Like, how fast can OCISLY return B1049 before going back out again for DM-2?

Maybe we will see JRTI back in action soon.

I believe that there has been a pretty quick turnaround time for OCISLY in the past. It was mentioned previously on the first page of this thread. I had thought that maybe they wanted to test JRTI for this mission and keep OCISLY for DM-2.

Also DM-2 might have a closer ASDS landing than a Starlink mission.
« Last Edit: 05/15/2020 04:32 pm by anof »

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #47 on: 05/15/2020 05:47 pm »
Will SpaceX be able to do the nine-day turnaround if Starlink goes off on Monday? Like, how fast can OCISLY return B1049 before going back out again for DM-2?

Maybe we will see JRTI back in action soon.

I believe that there has been a pretty quick turnaround time for OCISLY in the past. It was mentioned previously on the first page of this thread. I had thought that maybe they wanted to test JRTI for this mission and keep OCISLY for DM-2.

Also DM-2 might have a closer ASDS landing than a Starlink mission.

I know that already. According to Raul’s SpaceX map, the ASDS landing zone is 510 km downrange.
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May, 2020
« Reply #48 on: 05/15/2020 06:22 pm »
From the first page:

I'm surprised this is launching so close to DM-2 given that both are ASDS landings. There are only nine days to return the Starlink 8 booster to port, unload it, and get to the DM-2 booster landing site.
Nusantara Satu and DM-1 were just 8 days apart, they managed to do it but it was a very quick turn around from booster unloading to departure. They should be able to do a 9 day turnaround and a delay of 3 days should help them. But it would be a lot more helpful to have JRTI used this mission.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #49 on: 05/15/2020 10:37 pm »
https://twitter.com/spacexfleet/status/1261422930426298368

Quote
Fleet Update!

Of Course I Still Love You should arrive at the landing zone overnight tonight.

Ms. Tree and Ms. Chief are close behind and moving faster - they'll arrive around the same time.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #51 on: 05/16/2020 02:29 pm »
ULA just scrubbed with a 24 hour turnaround until after 9AM on the 17th. Expect a slip here.
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 17, 2020
« Reply #52 on: 05/16/2020 02:46 pm »
ULA just scrubbed with a 24 hour turnaround until after 9AM on the 17th. Expect a slip here.
Wonder how long until SpaceX cancels.  So much for an awesome weekend of space flight. Again.  :(
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 18, 2020
« Reply #53 on: 05/16/2020 03:01 pm »
May 16 launch of Atlas V scrubbed due to weather.  Team is performing a 24 hour turn-around for a launch on May 17.

This would move the Falcon 9 launch to its backup day on May 18.
« Last Edit: 05/16/2020 03:41 pm by zubenelgenubi »
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 18, 2020
« Reply #54 on: 05/16/2020 03:18 pm »
Confirmation

https://twitter.com/spacex/status/1261677306159890432

Quote
Due to a conflict on the Range, now targeting Monday, May 18 at 3:32 a.m. EDT for launch of Starlink

Edit to add:

https://twitter.com/julia_bergeron/status/1261688715631644674

Quote
Psst SpaceX is standing down with Atlas having Range priority. This tweet should actually say thank you for the weather delay to give our Recovery teams better recovery zone conditions at T-0. Fixed it for you.
« Last Edit: 05/16/2020 04:14 pm by FutureSpaceTourist »

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 18, 2020
« Reply #55 on: 05/16/2020 06:54 pm »
L-2 launch weather forecast for Monday now 90% GO

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 18, 2020
« Reply #56 on: 05/16/2020 09:47 pm »
https://twitter.com/thejackbeyer/status/1261770447277846529

Quote
The chances of recovery for Monday morning's Starlink launch are looking quite slim. Tropical Depression One will be located right over the recovery zone at T-0. The Fleet is already retreating towards safer waters on the coast. #SpaceXFleet

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 18, 2020
« Reply #57 on: 05/16/2020 10:19 pm »
Given the weather forecast, perhaps a delay to the May 19 launch window would be a better choice to maintain the opportunity to recover the booster?
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 19, 2020
« Reply #58 on: 05/17/2020 01:12 am »
https://twitter.com/spacex/status/1261818457810710529

Quote
Due to a tropical depression developing off the Southeast Coast of the U.S., now targeting Tuesday, May 19 at 3:10 a.m. EDT for the Starlink mission—SpaceX teams will continue monitoring launch and landing weather conditions

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 19, 2020
« Reply #59 on: 05/17/2020 07:46 am »
https://twitter.com/julia_bergeron/status/1261900909795323904

Quote
Go Ms. Tree just changed the reported destination to Tesla N Texas. They actually just arrived in Morehead City for safe harbor. I think whoever is at the wheel had a bit too much fun riding the waves. 😏 #SpaceXFleet

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 19, 2020
« Reply #60 on: 05/17/2020 03:29 pm »
L-2 weather forecast for Tuesday is 70% GO

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : May 19, 2020
« Reply #61 on: 05/17/2020 03:44 pm »
https://twitter.com/SpaceXFleet/status/1262045213750628352

Quote
The recovery fleet is sheltering from Tropical Storm Arthur.

Ms. Tree and Ms. Chief are docked at the Port of Morehead City. GO Quest is arriving at Cape Fear and OCISLY is circling just offshore nearby.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #62 on: 05/17/2020 11:28 pm »
https://twitter.com/nextspaceflight/status/1262161843407085568
Quote
SpaceX's next launch will have crew onboard. The Starlink launch is in fact now postponed until after Demo-2 due to not enough time to turnaround OCISLY.

JRTI still has several weeks of trials ahead of it before it will be ready.
« Last Edit: 05/17/2020 11:28 pm by gongora »

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #63 on: 05/18/2020 12:53 am »
Thanks for the update; I was hoping Go fever wouldn't rear its ugly head, and it didn't.

Good call, SpaceX.

Have a good one,
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Offline Joffan

Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #64 on: 05/18/2020 07:03 am »
Just a shame SpaceX couldn't keep their Sunday slot. Atlas would very likely have been fine launching Monday.
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #65 on: 05/18/2020 07:48 am »
Just a shame SpaceX couldn't keep their Sunday slot. Atlas would very likely have been fine launching Monday.

On the other hand: The slightest glitch on the Starlink launch (fifth flight of a booster again) could have delayed SpX-DM2 due to further investigation. This schedule risk is now off the table.
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #66 on: 05/18/2020 01:12 pm »
https://twitter.com/spacex/status/1262367345185558528

Quote
Standing down from the Starlink mission, due to tropical storm Arthur, until after launch of Crew Demo-2
« Last Edit: 05/18/2020 01:12 pm by FutureSpaceTourist »

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #67 on: 05/18/2020 04:09 pm »
  I have to wonder about the loss of one old booster compared to the cost of delaying the whole system for two more weeks. Maybe they can catch up, but it seems like launch opportunities is the pacer right now.
 A barge is going to have an unexpected problem eventually, and this faith in everything going to plan is going to come back and bite them.
« Last Edit: 05/18/2020 04:12 pm by Nomadd »
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #68 on: 05/18/2020 04:17 pm »
I have to wonder about the loss of one old booster compared to the cost of delaying the whole system for two more weeks. Maybe they can catch up, but it seems like launch opportunities is the pacer right now.

Per the Starlink tracking thread, they need Launch 7 and one of either the 3rd set from Launch 5 to precess to the correct plane, or Launch 8 to insert directly to that plane. If the latter race is decided by less than a few weeks, delaying Launch 7 might have no effect.

Quote
A barge is going to have an unexpected problem eventually, and this faith in everything going to plan is going to come back and bite them.

Probably one reason why they are updating JRTI to help out.
« Last Edit: 05/18/2020 04:35 pm by envy887 »

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #69 on: 05/18/2020 04:18 pm »
Just a shame SpaceX couldn't keep their Sunday slot. Atlas would very likely have been fine launching Monday.

On the other hand: The slightest glitch on the Starlink launch (fifth flight of a booster again) could have delayed SpX-DM2 due to further investigation. This schedule risk is now off the table.
But that kind of logic reduces commercial crew safety.
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #70 on: 05/18/2020 04:28 pm »
Just a shame SpaceX couldn't keep their Sunday slot. Atlas would very likely have been fine launching Monday.

On the other hand: The slightest glitch on the Starlink launch (fifth flight of a booster again) could have delayed SpX-DM2 due to further investigation. This schedule risk is now off the table.
But that kind of logic reduces commercial crew safety.
If one launch pushed by weather concerns after DM2 reduces commercial crew safety, then surely just one launch also reduces safety and they should have two.  Actually, scratch that - they should have three...

Where does postponing a non-crew launch prior to a crewed launch not reduce commercial crew safety?
No, I’m saying that if one of the arguments for postponing Starlink is that it might fail (exposing a potential underlying problem in Falcon 9), that’s effectively arguing for schedule risk management by putting blinders on to potential crew risk problems.

I’m not arguing they HAVE to get more launch statistics now; if they have to delay for *other* reasons, that’s fine.  I’m arguing against risk-management-by-self-deception as that’s clearly a poor safety culture.
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #71 on: 05/18/2020 04:31 pm »
They pushed the launch back because DM-2 is more important. (delaying it would have greater consequences than delaying a Starlink launch)

Not because they are worried that launching this Starlink launch would expose a F9 problem.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #72 on: 05/18/2020 04:38 pm »
Just a shame SpaceX couldn't keep their Sunday slot. Atlas would very likely have been fine launching Monday.

On the other hand: The slightest glitch on the Starlink launch (fifth flight of a booster again) could have delayed SpX-DM2 due to further investigation. This schedule risk is now off the table.
But that kind of logic reduces commercial crew safety.
It's not a logic you'd ever express publicly, but it's one you might have if you think the customer is ridiculously overcautious.
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #73 on: 05/18/2020 04:42 pm »
No, I’m saying that if one of the arguments for postponing Starlink is that it might fail (exposing a potential underlying problem in Falcon 9), that’s effectively arguing for schedule risk management by putting blinders on to potential crew risk problems.
Sure, and re-reading your post, I see you are saying "the idea" as you quote it above, if the delay were done to assure schedule, would be a reduction in safety, which I can get behind.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #74 on: 05/18/2020 04:55 pm »
Its so important, that making sure everyone involved in DM2 has 100% one focus, and no distractions.

So in June there seems to be Starlink 8, GPS3, and Starlink 9. No Idea when Starlink 10 was planned.
So with SL8 locked and loaded, and waiting, SX must have been working on SL9 already, and in 3 weeks, could thy be preparing SL10 !

Could we see a record pad turn-around, and/or 3SL launches, or 4 launches in one month? Or other records. If both drone ships are ready by June, that could facilitate such antics! :-0

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #75 on: 05/18/2020 08:17 pm »
Re: the back and forth about how it would have been better for the Starlink launch to proceed on Sunday, May 17:

In the L-2 forecast, up-thread here, the forecast for May 17 had a 20% chance of a launch site weather violation.  However, in the "Additional Risk Criteria" lists the risk imposed by the weather in the booster landing zone as "High."

Opinion follows: Even if May 17 had been free to launch, SpaceX may have chosen not to launch because the chances of a successful booster recovery appeared to have been low.  TS Arthur certainly had the sea churned up on the 17th.
« Last Edit: 05/18/2020 08:21 pm by zubenelgenubi »
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #76 on: 05/18/2020 09:08 pm »
Just a shame SpaceX couldn't keep their Sunday slot. Atlas would very likely have been fine launching Monday.

On the other hand: The slightest glitch on the Starlink launch (fifth flight of a booster again) could have delayed SpX-DM2 due to further investigation. This schedule risk is now off the table.

Just to clarify:

1. In no way I wanted to suggest that this was a reason to postpone Starlink. (SpaceX would not reason that way.) It is just an inevitable consequence of doing so.

2. I explicitly mentioned that this is a fifth flight. As you know, recently there has been the problem with a fifth-flight booster which was solely related to engine refurbishment. Such problem cannot happen with DM-2, but it could happen with Starlink v1.0-L7. Missing the chance of such problems to happen does not compromize DM-2 saftey.

Bottom line: This Starlink slip DOES reduce the schedule risk of SpX-DM2 (this is what I wanted to point out), but there is no reason to believe that it does compromise DM-2 safety.
« Last Edit: 05/18/2020 09:21 pm by PM3 »
"Never, never be afraid of the truth." -- Jim Bridenstine

Offline wannamoonbase

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #77 on: 05/18/2020 09:38 pm »
Its so important, that making sure everyone involved in DM2 has 100% one focus, and no distractions.

So in June there seems to be Starlink 8, GPS3, and Starlink 9. No Idea when Starlink 10 was planned.
So with SL8 locked and loaded, and waiting, SX must have been working on SL9 already, and in 3 weeks, could thy be preparing SL10 !

Could we see a record pad turn-around, and/or 3SL launches, or 4 launches in one month? Or other records. If both drone ships are ready by June, that could facilitate such antics! :-0

Yep, will depend on recovery vessels.  Not a bad problem to have.
Starship, Vulcan and Ariane 6 have all reached orbit.  New Glenn, well we are waiting!

Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #78 on: 05/19/2020 03:29 pm »
What happens to the booster that was on the pad, now that its set to launch in June?  Do they take it down and bring it back to the barn?

Offline woods170

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #79 on: 05/19/2020 03:38 pm »
What happens to the booster that was on the pad, now that its set to launch in June?  Do they take it down and bring it back to the barn?
Yes. F9 will be rolled back into the barn for weather protection of rocket and payload.

Payload stack (including fairing) will also be de-mated and stored in vertical (upright) position. A Starlink stack doesn't like being stored horizontally for prolonged periods of time (sagging of the stack is just one concern).
« Last Edit: 05/19/2020 03:40 pm by woods170 »

Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #80 on: 05/19/2020 04:16 pm »
Yes. F9 will be rolled back into the barn for weather protection of rocket and payload.

Payload stack (including fairing) will also be de-mated and stored in vertical (upright) position. A Starlink stack doesn't like being stored horizontally for prolonged periods of time (sagging of the stack is just one concern).


Awesome!  Thanks for the response!

Offline wannamoonbase

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #81 on: 05/21/2020 11:22 pm »
What happens to the booster that was on the pad, now that its set to launch in June?  Do they take it down and bring it back to the barn?
Yes. F9 will be rolled back into the barn for weather protection of rocket and payload.

Payload stack (including fairing) will also be de-mated and stored in vertical (upright) position. A Starlink stack doesn't like being stored horizontally for prolonged periods of time (sagging of the stack is just one concern).

Also curious how long they can wait before they want to redo a static fire.

Is the cycle time on using the ASDS the limitation on spacing between flights?
Starship, Vulcan and Ariane 6 have all reached orbit.  New Glenn, well we are waiting!

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #82 on: 05/21/2020 11:27 pm »
Is the cycle time on using the ASDS the limitation on spacing between flights?

That seems to be the case right now.  They've been doing a lot of work refitting the other ASDS, so hopefully when that's up and running it will be less of a problem.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #83 on: 05/21/2020 11:44 pm »
What happens to the booster that was on the pad, now that its set to launch in June?  Do they take it down and bring it back to the barn?
Yes. F9 will be rolled back into the barn for weather protection of rocket and payload.

Payload stack (including fairing) will also be de-mated and stored in vertical (upright) position. A Starlink stack doesn't like being stored horizontally for prolonged periods of time (sagging of the stack is just one concern).

Also curious how long they can wait before they want to redo a static fire.

Is the cycle time on using the ASDS the limitation on spacing between flights?

It's the limitation on flights that can't do RTLS. It is a known bottleneck, which is why SpaceX is preparing a second droneship.

The reason they bother doing a SF is because it's a used core has just been going through reentry, landing and refurbishment.

I don't think they would redo the static fire. At least not for a low profile launch such as Starlink. After all, technically every launch starts with a mini- static fire - launch clamps only release if the on board computer says it's passed.

So unless there's additional cause to check out the rocket - because it's either brand new or just came back from space, why would they?





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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #84 on: 05/25/2020 10:28 pm »
Spaceflight experts:
What is the Falcon 9 history with respect to Static Fire "re-do's"?

Also, how quickly could this Starlink launch from SLC-40 follow a successful launch of DM2 from LC-39A?  Is it dependent on the turn-around of OCISLY?
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #85 on: 05/25/2020 11:52 pm »
https://twitter.com/nextspaceflight/status/1265055392528130048

Quote
McAleenan: The 30th and 31st look much less dynamic [in terms of weather.]

Koenigsmann: Next Starlink mission in early June depending on the droneship availability.

Offline russianhalo117

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #86 on: 05/26/2020 12:03 am »
Spaceflight experts:
What is the Falcon 9 history with respect to Static Fire "re-do's"?

Also, how quickly could this Starlink launch from SLC-40 follow a successful launch of DM2 from LC-39A?  Is it dependent on the turn-around of OCISLY?
Solely dependent on which ASDS becomes available. JRTI could see operations as early as June.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #87 on: 05/27/2020 11:55 am »
Possible launch dates:
2020-06-02 01:38 UTC
2020-06-03 01:17 UTC

Quote
ATLANTIC OCEAN - FLORIDA - CAPE CANAVERAL: EASTERN RANGE OP# X0056 FALCON 9
Eastern range will be conducting hazardous operations surface to unlimited within portions of Warning Areas W497A, W497B, W137F/G, W138E,
W139E/F, W140E, W122 and the following Hazard Areas.

A: From 2836 55.22N 8036 0.35W
TO 2848N 8024W
TO 2854N 8017W
TO 2917N 7949W
TO 2915N 7946W
TO 2841N 8017W
TO 2834N 8025W
TO 2831N 8031W
TO 2830 25.65N 8033 0.42W to beginning

B: From 3158N 7658W
TO 3309N 7558W
TO 3323N 7536W
TO 3323N 7456W
TO 3315N 7437W
TO 3248N 7435W
TO 3229N 7459W
TO 3140N 7642W to beginning

Hazard periods for primary launch day and backup launch days;
Primary launch day: 02 / 0133Z thru 02 / 0331Z Jun 20. Preferred T-0 is 0138Z.
Backup launch day: 03 / 0112Z thru 03 / 0310Z Jun 20. Preferred T-0 is 0117Z.

https://www.navcen.uscg.gov/pdf/lnms/lnm07212020.pdf

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #88 on: 05/27/2020 12:03 pm »
Even if Crew Demo-2 launches today, using OCISLY for this mission would require ASDS turnaround of less than 6 days.

JRTI has done some sea runs recently, so it may indicate it's ready to support Starlink-8.
« Last Edit: 05/27/2020 12:04 pm by Elthiryel »
GO for launch, GO for age of reflight

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #89 on: 05/27/2020 03:17 pm »
We will know JRTI is ready for action when we see the SpaceX logo on the deck refreshed.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #90 on: 05/29/2020 05:52 pm »
Any activity at SLC-40 preparing for this launch?
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #91 on: 05/30/2020 09:34 pm »
JRTI has departed in what is believed to be for Starlink 8

https://twitter.com/SpaceXFleet/status/1266840103533584384

Quote
SpaceX's second droneship is now departing Port Canaveral.
'Just Read the Instructions' has been under construction for the past few months but is now all-but complete.
This is unrelated to today's Demo-2 mission.

Quote
Believe this will be in support of the previously postponed Starlink mission. Possible launch dates are:
2020-06-02 at 01:38 UTC
2020-06-03 at 01:17 UTC

Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #92 on: 05/30/2020 09:47 pm »
No guarantees on that tweet as I say. I'm pulling the info from the same mariner notices you'll are looking at.

Offline wannamoonbase

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #93 on: 05/30/2020 10:26 pm »
Excellent love the tenacity, can’t wait to see JRTI in action.

Every Starlink launch brings the Beta test closer. 
Starship, Vulcan and Ariane 6 have all reached orbit.  New Glenn, well we are waiting!

Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #94 on: 05/31/2020 01:42 am »
No guarantees on that tweet as I say. I'm pulling the info from the same mariner notices you'll are looking at.

Droneship trajectory now matches the LZ position of the previously postponed Starlink launch so I am willing to stick my neck out on a Starlink launch this coming week.

Offline Michael Baylor

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #95 on: 05/31/2020 02:23 am »
Launch NET June 3rd with a JRTI recovery, per NSF L2.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET June 3, 2020
« Reply #96 on: 05/31/2020 04:30 pm »
L-3 launch weather forecast is 80% GO
« Last Edit: 05/31/2020 04:31 pm by FutureSpaceTourist »

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : June 2020
« Reply #97 on: 05/31/2020 06:11 pm »
Any activity at SLC-40 preparing for this launch?
Following DM2's successful launch on May 30 from LC-39A, any activity at SLC-40? Preparations for a static fire?
Support your local planetarium! (COVID-panic and forward: Now more than ever.) My current avatar is saying "i wants to go uppies!" Yes, there are God-given rights. Do you wish to gainsay the Declaration of Independence?

Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET June 3, 2020
« Reply #98 on: 05/31/2020 06:17 pm »
If they don't static again will this be the first time they de stack and then fly without a new one?

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET June 3, 2020
« Reply #99 on: 05/31/2020 06:18 pm »
Any activity at SLC-40 preparing for this launch?
Following DM2's successful launch on May 30 from LC-39A, any activity at SLC-40? Preparations for a static fire?
Didn’t they already have a static fire before the launch was delayed? There is probably no need for another given the relatively short delay.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET June 3, 2020
« Reply #100 on: 05/31/2020 06:51 pm »
Any activity at SLC-40 preparing for this launch?
Following DM2's successful launch on May 30 from LC-39A, any activity at SLC-40? Preparations for a static fire?
Didn’t they already have a static fire before the launch was delayed? There is probably no need for another given the relatively short delay.
Yes. Thanks for the reminder.
Assuming no need for a repeat static fire:
From the point of view of an interested external observer, with no inside information, the first cue may be from off-site cameras, showing an erect Falcon 9 at SLC-40, on launch day.
« Last Edit: 06/01/2020 07:12 pm by zubenelgenubi »
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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET June 3, 2020
« Reply #101 on: 05/31/2020 08:03 pm »
http://www.launchphotography.com/Delta_4_Atlas_5_Falcon_9_Launch_Viewing.html
Quote
The next SpaceX Falcon 9 rocket from Cape Canaveral will launch the eighth batch of Starlink internet satellites from pad 40 on June 3 at about 9:25pm EDT.

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET June 3, 2020
« Reply #102 on: 05/31/2020 10:30 pm »
https://twitter.com/spacexfleet/status/1267219898964553730

Quote
Of Course I Still Love You is returning from the Demo-2 mission with Falcon 9.

Just Read the Instructions is en-route to the landing zone for the Starlink mission.

This is the first time that SpaceX has operated two droneships in the same ocean simultaneously for real missions.
« Last Edit: 05/31/2020 10:30 pm by FutureSpaceTourist »

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET June 3, 2020
« Reply #103 on: 06/01/2020 01:07 pm »
https://twitter.com/spacexfleet/status/1267440900671713281

Quote
Ms. Tree and Ms. Chief are preparing to depart Port Canaveral for the Starlink mission.

Edit to add:

https://twitter.com/shoredigmedia/status/1267445039577382912

Quote
Here they are departing now just passing Grills.
« Last Edit: 06/01/2020 01:31 pm by FutureSpaceTourist »

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Re: SpaceX F9 : Starlink 8 (v1.0 L7) : NET June 3, 2020
« Reply #104 on: 06/01/2020 02:25 pm »
L-2 weather forecast slightly worsened to 70% GO

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020
« Reply #105 on: 06/02/2020 01:14 pm »
L-1 launch weather forecast remains 70% GO

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020
« Reply #106 on: 06/02/2020 07:52 pm »
https://twitter.com/spacexfleet/status/1267906660774957056

Quote
Just Read the Instructions droneship has arrived at the landing zone for the Starlink mission.

...2 hours after OCISLY returned with the Demo-2 booster...

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020
« Reply #107 on: 06/02/2020 08:17 pm »
Is that 8:55 pm Eastern time tomorrow?  ???
"DARPA Hard"  It ain't what it use to be.

Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020
« Reply #108 on: 06/02/2020 08:20 pm »
Is that 8:55 pm Eastern time tomorrow?  ???
yes

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020
« Reply #109 on: 06/02/2020 08:32 pm »
Is that 8:55 pm Eastern time tomorrow?  ???
yes


The Manifest thread shows T-0 at 9:25 Eastern tomorrow. 

Summer evening launches can be really beautiful, don't miss this one.
Starship, Vulcan and Ariane 6 have all reached orbit.  New Glenn, well we are waiting!

Offline Mammutti

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020
« Reply #110 on: 06/02/2020 08:48 pm »
Quote
ATLANTIC OCEAN - FLORIDA - CAPE CANAVERAL: EASTERN RANGE OP# X0056 FALCON 9 STARLINK V1.0-L7 (UPDATE: 30 May, 2020)

Eastern range will be conducting hazardous operations surface to unlimited within portions of Warning Areas W497A, W497B, W137F/G, W138E,
W139E/F, W140E, W122 and the following Hazard Areas.

A: From 2836 55.22N 8036 0.35W
TO 2848N 8024W
TO 2854N 8017W
TO 2917N 7949W
TO 2915N 7946W
TO 2841N 8017W
TO 2834N 8025W
TO 2831N 8031W
TO 2830 25.65N 8033 0.42W to beginning

B: From 3158N 7658W
TO 3309N 7558W
TO 3323N 7536W
TO 3323N 7456W
TO 3315N 7437W
TO 3248N 7435W
TO 3229N 7459W
TO 3140N 7642W to beginning

Hazard periods for primary launch day and backup launch days;
Primary launch day: 04 / 0050Z thru 04 / 0248Z Jun 20. Preferred T-0 is 0055Z.
Backup launch day: 05 / 0028Z thru 05 / 0226Z Jun 20. Preferred T-0 is 0033Z.

https://www.navcen.uscg.gov/pdf/lnms/lnm07222020.pdf

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020
« Reply #111 on: 06/02/2020 11:19 pm »
https://twitter.com/TSKelso/status/1267906034338652161
Quote
CelesTrak now has pre-launch SupTLEs for the #Starlink-8 launch scheduled for Jun 4 at 0125 UTC from Cape Canaveral: https://celestrak.com/NORAD/elements/supplemental/.

Offline Ronsmytheiii

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020
« Reply #112 on: 06/03/2020 07:13 am »
As on the last pass on 2 June, Falcon 9 still not visible on SLC-40 via Sentinel-2 imagery:


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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020
« Reply #113 on: 06/03/2020 01:11 pm »
They are not providing press kits anymore ...

EDIT: Modified the document to include a link to the source website.

Good job! Thank you!

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020
« Reply #114 on: 06/03/2020 01:43 pm »
I have been thinking of doing something like what I attached, basically a long screenshot of the launches page converted to pdf. Main problem is that it starts as a png file, so the text is part of the image. I could find any tool that wouldn't leave out some parts or leave some glitches so if anyone knows a better tool that can do that, let us know!

Offline wannamoonbase

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Re: Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Updates
« Reply #115 on: 06/03/2020 02:07 pm »
They are not providing press kits anymore (Hillary Coe, Design Director at SpaceX, told me on Twitter that the launches site is going to replace the press kits, but she deleted that tweet :( ), so I decided to create my own press kit based on the information they provided on the website to have it saved for the future when they modify the website for another launch.

EDIT: Modified the document to include a link to the source website.

Thank you for producing this fan based press kit.  I like the support from fellow space fans.  Every launch is a great launch.
Starship, Vulcan and Ariane 6 have all reached orbit.  New Glenn, well we are waiting!

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #116 on: 06/03/2020 02:40 pm »
Visual profile for this launch

Offline rsdavis9

Does anybody have a ground position for 2nd stage cutoff. SECO? I was wondering if it would be visible from seacoast NH?
With ELV best efficiency was the paradigm. The new paradigm is reusable, good enough, and commonality of design.
Same engines. Design once. Same vehicle. Design once. Reusable. Build once.

Offline EspenU

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #118 on: 06/03/2020 07:40 pm »
Question is if the weather looks like in the picture below, can the F9 gain altitude fast enough to get above the storms and squeak thru?
It's out of the atmosphere within a couple of minutes. So I don't think gaining altitude quickly is an issue.

Offline ejb749

Current 12z run of weather around the launch site at 10pm Eastern.

Question is if the weather looks like in the picture below, can the F9 gain altitude fast enough to get above the storms and squeak thru?
I think the issue would be lightning in the area.

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #120 on: 06/03/2020 09:32 pm »
Before I steer people in my neighborhood wrong, am I correct in thinking there should be an excellent sighting opportunity in the central United States about 90 minutes after launch (i.e., around 10:00pm local time?)

Offline cppetrie

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #121 on: 06/03/2020 09:36 pm »
Before I steer people in my neighborhood wrong, am I correct in thinking there should be an excellent sighting opportunity in the central United States about 90 minutes after launch (i.e., around 10:00pm local time?)
Check heavens-above.com for your location to confirm passes. They have a placeholder for L7 on their homepage. For southern MN the first visible evening pass is tomorrow night at 10:08 PM.

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #122 on: 06/03/2020 09:43 pm »
Check heavens-above.com for your location to confirm passes. They have a placeholder for L7 on their homepage. For southern MN the first visible evening pass is tomorrow night at 10:08 PM.

Thanks! I didn't expect they'd have sighting opportunities prepared before launch.
West Texas does have a sighting opportunity from 10:00 to 10:01 tonight.

Offline cppetrie

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #123 on: 06/03/2020 09:54 pm »
Check heavens-above.com for your location to confirm passes. They have a placeholder for L7 on their homepage. For southern MN the first visible evening pass is tomorrow night at 10:08 PM.

Thanks! I didn't expect they'd have sighting opportunities prepared before launch.
West Texas does have a sighting opportunity from 10:00 to 10:01 tonight.
SpaceX has been providing prelaunch supplemental TLEs to tracking sites so they can calculate passes even before launch. It’s pretty awesome that all parties are working together to provide pass data ahead of launch. Having seen the Starlink train after the last launch it is really quite a spectacular sight to see.

Offline leetdan

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #124 on: 06/03/2020 10:42 pm »
There's a fun side-effect of those pre-published TLEs... Here in Central Florida, we'll have the chance to see the train of satellites rise above the southwest horizon a mere 150 seconds after launch! ???

Offline Prettz

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #125 on: 06/04/2020 01:30 am »
I might have missed it, but did they say if these fairing halves are used?

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #126 on: 06/04/2020 01:34 am »
Another one on the deck... amazing :)

Edit... had to attach pics of landing since it was cloudy here and I couldn't see liftoff :|
« Last Edit: 06/04/2020 01:42 am by webdan »

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #127 on: 06/04/2020 01:37 am »
And the drone ship feed did NOT cut out at all. Very smooth during the whole landing burn.
Liftoff for St. Jude's! Go Dragon, Go Falcon, Godspeed Inspiration4!

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #128 on: 06/04/2020 01:37 am »
Number 5! Congrats SpaceX!

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #129 on: 06/04/2020 01:41 am »
OMG we saw it deploy!!!!!!!

Offline AndrewRG10

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #130 on: 06/04/2020 01:42 am »
Wonder what they've been wanting to hide for so long? Glad they did show it though.

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #131 on: 06/04/2020 01:42 am »
THERE WAS NO BLIP! NO BLIP!!

[Seinfeld]

Offline mjcrsmith

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #132 on: 06/04/2020 01:44 am »
Great video on this launch and landing.  Guessing JRTI had its system upgraded on the referb.

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #133 on: 06/04/2020 01:48 am »
Quite a week SpaceX, congrats! 8)
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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #134 on: 06/04/2020 01:50 am »
Best launch video
Wonder what they've been wanting to hide for so long? Glad they did show it though.

Maybe the fact that they produces space debris by jetisoning the clamp?

Offline CorvusCorax

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #135 on: 06/04/2020 01:50 am »
WOW. They actually showed the deployment this time :-) So fascinating :)

I wonder if the fact that OneWeb as the main competitor has gone bankrupt has anything to do with it. Probably not, they never had the architecture to even try and adapt to this. Blue Origin possibly could, if Kuiper eventually becomes reality, but then again by the looks of it Starlink will probably be on-line and serve customers before Blue Origin makes their first successful orbital launch.

I think, when your technological lead has become far enough that even a fast follower would take years to get to where you are now, you can show your tricks safely, knowing that by the time someone could duplicate them, you wont need them anymore.

Specifically in this case, by the time Kuiper sats could benefit from a bulk deployer on top of New Shepperd Glenn SpaceX would already shovel them out of Starships cargo hold in bulk quantities with an entirely different method.

If this deployer has been compared to a dump truck dumping its load versus individual offloading of palettes, then what Starship might be doing could be closer to pressure pumping concrete through a construction pipeline...

« Last Edit: 06/04/2020 01:52 am by CorvusCorax »

Offline TorenAltair

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #136 on: 06/04/2020 01:53 am »
Stage and sats just passed nearly overhead here. Clearly visible through dispersing remnants of rain clouds.

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #137 on: 06/04/2020 01:53 am »
WOW. They actually showed the deployment this time :-) So fascinating :)

I wonder if the fact that OneWeb as the main competitor has gone bankrupt has anything to do with it. Probably not, they never had the architecture to even try and adapt to this. Blue Origin possibly could, if Kuiper eventually becomes reality, but then again by the looks of it Starlink will probably be on-line and serve customers before Blue Origin makes their first successful orbital launch.

I think, when your technological lead has become far enough that even a fast follower would take years to get to where you are now, you can show your tricks safely, knowing that by the time someone could duplicate them, you wont need them anymore.

Specifically in this case, by the time Kuiper sats could benefit from a bulk deployer on top of New Shepperd Glenn SpaceX would already shovel them out of Starships cargo hold in bulk quantities with an entirely different method.

If this deployer has been compared to a dump truck dumping its load versus individual offloading of palettes, then what Starlink might be doing could be closer to pressure pumping concrete through a construction pipeline...

I must admit, I briefly considered the "hey Oneweb just went bankrupt" angle as well, but I'll stick with "unexpected interference due to shock/moving metal that they've only just worked around" for now.
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Offline CorvusCorax

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #138 on: 06/04/2020 02:01 am »
WOW. They actually showed the deployment this time :-) So fascinating :)

I wonder if the fact that OneWeb as the main competitor has gone bankrupt has anything to do with it. Probably not, they never had the architecture to even try and adapt to this. Blue Origin possibly could, if Kuiper eventually becomes reality, but then again by the looks of it Starlink will probably be on-line and serve customers before Blue Origin makes their first successful orbital launch.

I think, when your technological lead has become far enough that even a fast follower would take years to get to where you are now, you can show your tricks safely, knowing that by the time someone could duplicate them, you wont need them anymore.

Specifically in this case, by the time Kuiper sats could benefit from a bulk deployer on top of New Shepperd Glenn SpaceX would already shovel them out of Starships cargo hold in bulk quantities with an entirely different method.

If this deployer has been compared to a dump truck dumping its load versus individual offloading of palettes, then what Starlink might be doing could be closer to pressure pumping concrete through a construction pipeline...

I must admit, I briefly considered the "hey Oneweb just went bankrupt" angle as well, but I'll stick with "unexpected interference due to shock/moving metal that they've only just worked around" for now.

Apropos working around RF interference - they also managed uninterrupted landing coverage from JRTI - after it has just been refitted extensively. I hope that wasn't a fluke but points to a more robust architecture.

After all SpaceX IS deploying a global communication network at this very time, if there's one thing they should be able to deliver, then it's uninterrupted coverage from anywhere in the world ;)

At this point it might even be possible that the new droneship has an experimental Starlink transceiver.

But F9 probably would need new FCC documents to do so - unless Starlinks just happen to be able to receive and relay F9 telemetry ;)

Offline ClayJar

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #139 on: 06/04/2020 02:09 am »
Wonder what they've been wanting to hide for so long? Glad they did show it though.

Maybe the fact that they produces space debris by jetisoning the clamp?

Watching how relatively quickly the deployment rods decay and reenter, that idea never really made sense to me, but whatever reason (technical, procedural, or managerial) we finally got to see the deployment, I'm stoked.  Now I'm trying to work out how the deployment is actuated.  (Watching it repeatedly, you can see the deployment rods "slacken" before swinging out and releasing.)

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #141 on: 06/04/2020 02:41 am »
The curved bit in the middle looks like a mass to pull the rod outwards due to the deployment spin.

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #142 on: 06/04/2020 03:15 am »
Does anyone have a prediction for visibility for the first two passes over the US?
Particularly Denver
What kind of wastrels would dump a perfectly good booster in the ocean after just one use?

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #143 on: 06/04/2020 03:18 am »
Does anyone have a prediction for visibility for the first two passes over the US?
Particularly Denver

Saw nothing from west Texas. Expected Starlink very low in the SW, but the moon is very bright this evening.
The morning passes on Thursday and Friday look much more favorable.

Offline Lars-J

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #144 on: 06/04/2020 03:20 am »
With the mechanism as shown, I'm a bit surprised they did not design them to stay attached to the upper stage through a plain hinge. But on the other hand, perhaps there is a risk they could bounce back and re-contact the stack... And there are no doubt other concerns. I have no illusions about seeing things that did not occur to the team.  :) And this is cheap, and works.

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #145 on: 06/04/2020 04:02 am »
WOW. They actually showed the deployment this time :-) So fascinating :)

I wonder if the fact that OneWeb as the main competitor has gone bankrupt has anything to do with it. Probably not, they never had the architecture to even try and adapt to this. Blue Origin possibly could, if Kuiper eventually becomes reality, but then again by the looks of it Starlink will probably be on-line and serve customers before Blue Origin makes their first successful orbital launch.

I think, when your technological lead has become far enough that even a fast follower would take years to get to where you are now, you can show your tricks safely, knowing that by the time someone could duplicate them, you wont need them anymore.

Specifically in this case, by the time Kuiper sats could benefit from a bulk deployer on top of New Shepperd Glenn SpaceX would already shovel them out of Starships cargo hold in bulk quantities with an entirely different method.

If this deployer has been compared to a dump truck dumping its load versus individual offloading of palettes, then what Starlink might be doing could be closer to pressure pumping concrete through a construction pipeline...

I must admit, I briefly considered the "hey Oneweb just went bankrupt" angle as well, but I'll stick with "unexpected interference due to shock/moving metal that they've only just worked around" for now.

It's equally possible that someone is in really hot water now because they forgot to push the 'generate interference' button.

Offline geza

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #146 on: 06/04/2020 04:28 am »
Watching how relatively quickly the deployment rods decay and reenter, that idea never really made sense to me, but whatever reason (technical, procedural, or managerial) we finally got to see the deployment, I'm stoked.  Now I'm trying to work out how the deployment is actuated.  (Watching it repeatedly, you can see the deployment rods "slacken" before swinging out and releasing.)

It seems that there is a pusher (in white) in operation at the near end of the rod. Something like this must operate at the far end  also, as the rod starts to move upward parallelly. I  guess the pusher just contain a spring. A latching mechanism should keep it compressed before the commanded release. Also, the satellite stack seems to be pushed away by something. However, the stack is released only after the rod separation is complete. Therefore, stack release is either mechanically connected to rod release, or commended separately.

Offline jacobmarley

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #147 on: 06/04/2020 04:45 am »
Does anyone have a prediction for visibility for the first two passes over the US?
Particularly Denver
According to n2yo, overnight around 4:50 AM(denver time) from NW to SE or tomorrow at 21:05 PM from SW to NE !

Offline wxmeddler

I tried looking from here in Fargo at 23:38 local. This works this time of year because of our latitiude. Even with a 67 deg max elevation, didn't see anything. Usually can see ISS at ~420 km till midnight, but not sure with how low the stack (perigee 230) is if that is enough.

Offline CorvusCorax

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #149 on: 06/04/2020 10:41 am »
Watching how relatively quickly the deployment rods decay and reenter, that idea never really made sense to me, but whatever reason (technical, procedural, or managerial) we finally got to see the deployment, I'm stoked.  Now I'm trying to work out how the deployment is actuated.  (Watching it repeatedly, you can see the deployment rods "slacken" before swinging out and releasing.)

It seems that there is a pusher (in white) in operation at the near end of the rod. Something like this must operate at the far end  also, as the rod starts to move upward parallelly. I  guess the pusher just contain a spring. A latching mechanism should keep it compressed before the commanded release. Also, the satellite stack seems to be pushed away by something. However, the stack is released only after the rod separation is complete. Therefore, stack release is either mechanically connected to rod release, or commended separately.

Do not forget the entire stack is under tension due to the stage rotation around y axis.

Being not in the center of gravity, the satellites want to drift away from each other and the stage as opposed to remaining in rotation around a joint center of mass. A centripetal force acts through the rod, pulling the stack together. The moment the rods let lose, the sats will separate from each other and the stage simply by momentum already imparted to them.

Ultra simple, ultra effective. Part count: zero.


Offline niwax

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #150 on: 06/04/2020 11:24 am »
I tried looking from here in Fargo at 23:38 local. This works this time of year because of our latitiude. Even with a 67 deg max elevation, didn't see anything. Usually can see ISS at ~420 km till midnight, but not sure with how low the stack (perigee 230) is if that is enough.

If they already use the new orientation for ascent, we might see very little of these satellites if anything with the naked eye.
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Offline Jcc

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #151 on: 06/04/2020 11:44 am »
Watching how relatively quickly the deployment rods decay and reenter, that idea never really made sense to me, but whatever reason (technical, procedural, or managerial) we finally got to see the deployment, I'm stoked.  Now I'm trying to work out how the deployment is actuated.  (Watching it repeatedly, you can see the deployment rods "slacken" before swinging out and releasing.)

It seems that there is a pusher (in white) in operation at the near end of the rod. Something like this must operate at the far end  also, as the rod starts to move upward parallelly. I  guess the pusher just contain a spring. A latching mechanism should keep it compressed before the commanded release. Also, the satellite stack seems to be pushed away by something. However, the stack is released only after the rod separation is complete. Therefore, stack release is either mechanically connected to rod release, or commended separately.

Do not forget the entire stack is under tension due to the stage rotation around y axis.

Being not in the center of gravity, the satellites want to drift away from each other and the stage as opposed to remaining in rotation around a joint center of mass. A centripetal force acts through the rod, pulling the stack together. The moment the rods let lose, the sats will separate from each other and the stage simply by momentum already imparted to them.

Ultra simple, ultra effective. Part count: zero.

I was just wondering where the center of mass is for the stage2-starlink stack with mostly empty prop tanks. Estimates are that stage 2 has a mass of 4.5 tones at burnout. The starlink sats are more than that, so the axis of spin should be inside the starlink stack somewhere. So, a pusher mechanism to separate them from stage 2 is essential.

Offline XenIneX

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #152 on: 06/04/2020 12:51 pm »
I was just wondering where the center of mass is for the stage2-starlink stack with mostly empty prop tanks. Estimates are that stage 2 has a mass of 4.5 tones at burnout. The starlink sats are more than that, so the axis of spin should be inside the starlink stack somewhere. So, a pusher mechanism to separate them from stage 2 is essential.
Not at all.  Stop thinking in an S2-centric reference frame; it's a loosely-associated collection of objects, each with their own inertia.  If the second stage is outside the center of mass -- and thus the center of rotation -- it goes flying when the retention mechanism lets go, just like the satellite on the opposite end does.


Awful text art:

STAGE2
   
      sat
   ⬆    ⬆  sat     (center of mass/rotation)
   ⬆    ⬆   ⬆   
STAGE2 sat sat >< sat sat sat sat sat sat
                   ⬇   ⬇   ⬇   ⬇   ⬇   ⬇
                  sat  ⬇   ⬇   ⬇   ⬇   ⬇
                      sat  ⬇   ⬇   ⬇   ⬇
                          sat  ⬇   ⬇   ⬇
                              sat  ⬇   ⬇
                                  sat 
                                      sat
« Last Edit: 06/04/2020 01:01 pm by XenIneX »

Offline geza

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #153 on: 06/04/2020 02:38 pm »
It seems that there is a pusher (in white) in operation at the near end of the rod. Something like this must operate at the far end  also, as the rod starts to move upward parallelly. I  guess the pusher just contain a spring. A latching mechanism should keep it compressed before the commanded release. Also, the satellite stack seems to be pushed away by something. However, the stack is released only after the rod separation is complete. Therefore, stack release is either mechanically connected to rod release, or commended separately.

Do not forget the entire stack is under tension due to the stage rotation around y axis.

Being not in the center of gravity, the satellites want to drift away from each other and the stage as opposed to remaining in rotation around a joint center of mass. A centripetal force acts through the rod, pulling the stack together. The moment the rods let lose, the sats will separate from each other and the stage simply by momentum already imparted to them.

Ultra simple, ultra effective. Part count: zero.

This is not exactly what we see on the video. The stack of satelites separates together from the stage with a definite push, which is definitely delayed relative to the jettisoning of the rod.

Offline rsdavis9

Do we know the rotation is end over end?
I always assumed it was a roll.
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Online kdhilliard

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #155 on: 06/04/2020 02:50 pm »
This is not exactly what we see on the video. The stack of satellites separates together from the stage with a definite push, which is definitely delayed relative to the jettisoning of the rod.
That's what I thought at first, but looking again closely it appears that they start moving as soon as the rod is free, but with the upper satellites in the stack separating moving away more quickly than the lower ones.

Edit: Clarity
« Last Edit: 06/04/2020 03:16 pm by kdhilliard »

Offline eriblo

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #156 on: 06/04/2020 03:03 pm »
This is not exactly what we see on the video. The stack of satelites separates together from the stage with a definite push, which is definitely delayed relative to the jettisoning of the rod.
That's what I thought at first, but looking again closely it appears that they start moving as soon as the rod is free, but with the upper satellites in the stack separating more quickly than the lower ones.
I do not see any sign of a push either. Remember that the second stage center of mass is many meters back from the center of rotation while those of the satellites are only separated by the thickness of the satellites. You would therefore expect the stage to separate much more rapidly from the closest satellite than the satellites separate from each other.

Online kdhilliard

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #157 on: 06/04/2020 03:15 pm »
Do we know the rotation is end over end?
I always assumed it was a roll.
You can see the moon passing by in last night's mission about ten seconds before deployment, but the flat spin is even more visible in daylight.  Here is during March's Starlink 6 keyed to T+00:13:36.  The spin is visible for 70 seconds before the 30 second deployment cutaway.  Post-deployment, you can see the stage stabilize itself.

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #158 on: 06/04/2020 04:26 pm »
It seems that there is a pusher (in white) in operation at the near end of the rod. Something like this must operate at the far end  also, as the rod starts to move upward parallelly. I  guess the pusher just contain a spring. A latching mechanism should keep it compressed before the commanded release. Also, the satellite stack seems to be pushed away by something. However, the stack is released only after the rod separation is complete. Therefore, stack release is either mechanically connected to rod release, or commended separately.

Do not forget the entire stack is under tension due to the stage rotation around y axis.

Being not in the center of gravity, the satellites want to drift away from each other and the stage as opposed to remaining in rotation around a joint center of mass. A centripetal force acts through the rod, pulling the stack together. The moment the rods let lose, the sats will separate from each other and the stage simply by momentum already imparted to them.

Ultra simple, ultra effective. Part count: zero.

This is not exactly what we see on the video. The stack of satelites separates together from the stage with a definite push, which is definitely delayed relative to the jettisoning of the rod.
Is there any RCS capability to "tap the brakes"?

Offline whitelancer64

It seems that there is a pusher (in white) in operation at the near end of the rod. Something like this must operate at the far end  also, as the rod starts to move upward parallelly. I  guess the pusher just contain a spring. A latching mechanism should keep it compressed before the commanded release. Also, the satellite stack seems to be pushed away by something. However, the stack is released only after the rod separation is complete. Therefore, stack release is either mechanically connected to rod release, or commended separately.

Do not forget the entire stack is under tension due to the stage rotation around y axis.

Being not in the center of gravity, the satellites want to drift away from each other and the stage as opposed to remaining in rotation around a joint center of mass. A centripetal force acts through the rod, pulling the stack together. The moment the rods let lose, the sats will separate from each other and the stage simply by momentum already imparted to them.

Ultra simple, ultra effective. Part count: zero.

This is not exactly what we see on the video. The stack of satelites separates together from the stage with a definite push, which is definitely delayed relative to the jettisoning of the rod.
Is there any RCS capability to "tap the brakes"?

Yes, but it's not needed for deployment. Second stage stabilizes itself after separation, then deorbits some time later.
"One bit of advice: it is important to view knowledge as sort of a semantic tree -- make sure you understand the fundamental principles, ie the trunk and big branches, before you get into the leaves/details or there is nothing for them to hang on to." - Elon Musk
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Offline wannamoonbase

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #160 on: 06/04/2020 05:04 pm »
I've checked all the threads I can think of and the SpaceX twitter feed.

Is there any word on the fairing recovery attempt on last nights launch?
Starship, Vulcan and Ariane 6 have all reached orbit.  New Glenn, well we are waiting!

I've checked all the threads I can think of and the SpaceX twitter feed.

Is there any word on the fairing recovery attempt on last nights launch?
No, ships are heading back.

Offline RocketLover0119

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #162 on: 06/04/2020 05:07 pm »
I've checked all the threads I can think of and the SpaceX twitter feed.

Is there any word on the fairing recovery attempt on last nights launch?

Nope. Should be able to tell if they were fished or caught by the net they are sitting on. If they are sitting on the blue net they were caught, or the black net means they were fished.

Probably fished them judging by lack of communication though.
« Last Edit: 06/04/2020 05:08 pm by RocketLover0119 »
"The Starship has landed"

Offline Lars-J

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #163 on: 06/04/2020 06:12 pm »
This is not exactly what we see on the video. The stack of satelites separates together from the stage with a definite push, which is definitely delayed relative to the jettisoning of the rod.

Look closer. As soon as the rods clear (some connection at the top is broken), the satellites slowly start "falling away" due to the rotation. As for evidence on the rotation, note the moon in the shot (tiny dot due to wide angle), moving across the screen and reflecting of the stage/payload.

Offline ChrML

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #164 on: 06/04/2020 08:30 pm »
We already know SpaceX is pushing the envelope in terms of reuse count and rapid reuse with their own Starlink satellites.

But if launch windows and range availability becomes the largest constraint, could we see them pushing the envelope on the weather constraints? To see the actual limits and margins on the rocket.

They already said they're producing more satellites than they can launch.
« Last Edit: 06/04/2020 08:30 pm by ChrML »

Offline CorvusCorax

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #165 on: 06/04/2020 08:42 pm »
I was wondering the same thing considering last nights tight weather margins.

Falcon9 is a thin and long rocket, so its relatively vulnerable to wind shear, turbulence, etc... so I can't really see them launching through a proper thunderstorm cloud. Rain and hail is also not nice if you go though it supersonic and want to reuse your fairing.

But if it's just high static electricity field strengths? Why not.

It might actually be great data for NASA and other customers to have a few lightning strikes on non-customer-launches and see the effect on avionics, launch abort charges, payload, etc... just no customer wants to be the one to provide that data.

Offline wannamoonbase

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #166 on: 06/04/2020 08:54 pm »
We already know SpaceX is pushing the envelope in terms of reuse count and rapid reuse with their own Starlink satellites.

But if launch windows and range availability becomes the largest constraint, could we see them pushing the envelope on the weather constraints? To see the actual limits and margins on the rocket.

They already said they're producing more satellites than they can launch.

Doubtful, they'll stretch the weather limits too far.  The F9 does a great job getting off the pad on time when not weather constrained.  They can take a few delays here and there, all while queuing up the next launch.

The critical path for launch pace seems to be booster and ASDS availability.
Starship, Vulcan and Ariane 6 have all reached orbit.  New Glenn, well we are waiting!

Offline kessdawg

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #167 on: 06/04/2020 10:48 pm »
Also correct me if I'm wrong but I believe there are some weather constraints that will close the range regardless of rocket requirements.

Offline Steven Pietrobon

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #168 on: 06/05/2020 06:47 am »
Ultra simple, ultra effective. Part count: zero.

Part count is at least four, since there are four hold down posts that are released and left to decay in LEO.
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Offline Lars-J

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #169 on: 06/05/2020 08:17 am »
Ultra simple, ultra effective. Part count: zero.

Part count is at least four, since there are four hold down posts that are released and left to decay in LEO.
Four? Explain your logic there. There appears to be only two pieces that separate from the upper stage. And satellite / debris tracking confirms that.

Offline Elthiryel

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #170 on: 06/05/2020 08:40 am »
No, actually tracking confirms it's four (despite the fact that looking at the stream I would also say it's two). Here's the example from launch 7, but it's the same for each of them.

https://twitter.com/planet4589/status/1263692953467457536
« Last Edit: 06/05/2020 04:37 pm by Elthiryel »
GO for launch, GO for age of reflight

Offline haywoodfloyd

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TLE File for Starlink-7
« Reply #171 on: 06/05/2020 01:08 pm »
I'm not sure where to post this so feel free to move it.
Does anyone know where I could find the TLE file containing  the newest Starlink satellites so I can download it to Stellarium?
Or alternately what the designations of the satellites are/will be (STARLINK-XXXX)?
Thanks
« Last Edit: 06/05/2020 01:11 pm by haywoodfloyd »

Offline Elthiryel

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Re: TLE File for Starlink-7
« Reply #172 on: 06/05/2020 01:27 pm »
All objects with the international designator starting with 2020-035 are the objects from the last Starlink launch (Starlink-8 or Starlink V1.0 L7).

http://celestrak.com/NORAD/elements/supplemental/table.php?tleFile=starlink&title=Starlink&orbits=0&pointsPerRev=90&frame=1
« Last Edit: 06/05/2020 01:30 pm by Elthiryel »
GO for launch, GO for age of reflight

Offline haywoodfloyd

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Re: TLE File for Starlink-7
« Reply #173 on: 06/05/2020 02:13 pm »
Thank you very much Elthiryel.

Offline rsdavis9

Anybody know if S2 reentered already?
I saw the sats last night and one was bright continuous and one flashed briefly. So assume the one bright was the S2? I couldn't find the S2 in heavens above search. A lot of them appear as
"FALCON 9 DEB"
but none of them had a launch date of the Jun 4th.
With ELV best efficiency was the paradigm. The new paradigm is reusable, good enough, and commonality of design.
Same engines. Design once. Same vehicle. Design once. Reusable. Build once.

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #175 on: 06/07/2020 06:38 pm »
I hadn’t remembered that B1049 and JRTI have history ...

Quote
The only time B1049 returned to port aboard Just Read the Instructions was on the West coast following the Iridium-8 mission. Today, the same booster is again set to arrive aboard JRTI, but this time on the EAST coast, after its FIFTH successful launch and landing. #spacex

https://twitter.com/spacexfleet/status/1269699906081521666

Offline kessdawg

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #177 on: 06/09/2020 10:35 pm »
Starlink fairing deploy sequence

https://twitter.com/SpaceX/status/1270466922459459590

twitter.com/djsnm/status/1270470538553679877

Quote
Things to see here:
* Watch for the fairing flexing after separation.
* It falls out away from rocket, then rear half gets kicked by the exhaust, reversing the rotation.
* The limb of the earth is visible as a reflection in side of satellite stack.

https://twitter.com/djsnm/status/1270470539564519425

Quote
* the parachute likes and steering hardware are all visible, see how the lines are laid out inside the fairing.
* Probably the best shot we've ever see of Merlin Vacuum in flight.
* The blue exhaust from illumination by the sun
* A view of the exhaust trail from inside!

Offline Alexphysics

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #178 on: 06/10/2020 02:22 am »
Funny how SpaceX calls this mission just "Starlink 7" considering all the fights people have had about calling these either by their flight number or just the number of flights of the version they're in. During old times I defended using "Starlink #" with the number being the flight number within the v1.0 version since that's what appears on official documentation and internally by SpaceX. Many others thought that it was better to just number them in flight order instead so this one would have been Starlink 8 not Starlink 7. I stopped caring about this right after Starlink v1.0 L2 because it's just stupid. But just letting you know again that SpaceX, even to this day, still considers v0.9 an experiment and sort of like "flight 0". It feels good to be right from time to time :P

Offline tyrred

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #179 on: 06/10/2020 08:58 am »


And here it is on you tube.

Mesmerizing.

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Re: SpaceX F9 : Starlink v1.0 L7 : June 3/4, 2020 : Discussion
« Reply #180 on: 06/12/2020 07:30 pm »


Quote
On Tuesday a great video was posted from the fairing of a SpaceX rocket carrying a payload of Starlink Satellites. It was one of the best looks at the interior of the fairings which are practically independent spacecraft able to control their entry & descent to steer their way to a rendezvous with the recovery vessels.

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