Author Topic: SpaceX F9 : Astranis Block 2 : CCSFS SLC-40 : 29 December 2024 (05:00 UTC)  (Read 59408 times)

Offline FutureSpaceTourist

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https://twitter.com/spacex/status/1873264807253819692

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Falcon 9 completes back-to-back missions from California and Florida, delivering 22 @Starlink satellites to the constellation and @Astranis’s From One to Many mission to orbit on our 132nd and 133rd launches of the year

Offline FutureSpaceTourist

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https://twitter.com/gedmark/status/1873278331468062975

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Great news-- we have acquired and established command authority over all four spacecraft.

We'll keep you all posted as these missions continue to progress.

Thanks for the ride, @SpaceX. Hell of a launch.

Offline zubenelgenubi

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Congratulations to all team members on a successful launch campaign! 👏 🙌 👍

Thank you, NSF webcasters! 🌟🎊

Thank you, FST, for tonight's launch thread coverage! ✨️ 😀

Next, the third leg of the Falcon 9 launch triad or threepeat on December 30!
« Last Edit: 12/29/2024 04:50 pm by zubenelgenubi »
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Offline FutureSpaceTourist

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Slo-mo video:

https://twitter.com/_mgde_/status/1873391023189078446

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Liftoff of Falcon 9 and its payload of 4 MicroGEO satellites for @Astranis from Pad 40.

Mega night for all teams involved!

📸 - @NASASpaceflight

📺 - youtube.com/live/a5lxyXToh…


Doug returned to PC on Dec 24 @ 4:08pm ET

Doug departed PC on Dec 26 @ 8:14pm ET

Doug returned to PC on Dec 30 @ 7:18pm ET


Signet Warhorse I + ASOG returned to PC on Dec 23 @ 1:29pm ET post abort

Signet Warhorse I + ASOG departed PC on Dec 26 @ 5:37pm ET

Signet Warhorse I + ASOG + B1083 returned to PC on Dec 30 @ 8:04pm ET

Offline cpushack

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22nd! flight for one fairing, 12 for the other

Online catdlr

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It's Tony De La Rosa, ...I don't create this stuff, I just report it.

Offline shiro

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Some reusability stats for this launch (Astranis Block 2):

Booster B1083.7 turnaround time:
29 days 0 hours 0 minutes
(its previous mission was Starlink Group 6-65 on Nov 30, 2024 UTC).

FYI: median turnaround time for Falcon 9 / Heavy boosters is currently 29.34 days *
* – based on the last 30 launches, excluding new first stages.

Launchpad SLC-40 turnaround time:
12 days 4 hours 8 minutes
(the previous launch from this pad was GPS III-07 (Sally Ride) on Dec 17, 2024 UTC).

FYI: median turnaround time for SLC-40 is currently 5.17 days *
* – based on the last 30 launches.

The same type of stats for previous SpaceX launches may be found on this spreadsheet online.

Online GewoonLukas_

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1469 m/s to GEO:

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We got dropped off at an orbit that is approximately 400km x 65,000km x 12.5 deg inclination

We primarily used the extra performance to reduce inclination. Turned out to be optimal for a shorter electric orbit raise.

https://twitter.com/Gedmark/status/1875975379791552754
Lukas C. H. • Hobbyist Mission Patch Artist 🎨 • May the force be with you my friend, Ad Astra Per Aspera ✨️

Offline ZachS09

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Actually, less than 1,469 m/s.
« Last Edit: 01/05/2025 11:59 pm by ZachS09 »
Liftoff for St. Jude's! Go Dragon, Go Falcon, Godspeed Inspiration4!

Offline Steven Pietrobon

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Actually, less than 1,469 m/s.

Here's the current version of my orbit program, which gives the following output.

Delta-V calculator by Steven S. Pietrobon. 25 Nov 2022.
Enter negative initial perigee height to exit program.
Enter negative required height for geosynchronous altitude.

Enter initial perigee height (km): 400
Enter initial apogee height (km): 65000
Enter required inclination change (°): 12.5
Enter required perigee height (km): -1
Geosynchronous perigee = 35786.0 km
Enter required apogee height (km): -1
Geosynchronous apogee = 35786.0 km

Burn at 65000.0 km: theta1 = 11.74°, dv1 = 1091.4 m/s
Burn at 35786.0 km: theta2 =  0.76°, dv2 =  375.5 m/s
dv = 1466.9 m/s
Saved 2.6 m/s
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Offline ZachS09

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Actually, less than 1,469 m/s.

Here's the current version of my orbit program, which gives the following output.

Delta-V calculator by Steven S. Pietrobon. 25 Nov 2022.
Enter negative initial perigee height to exit program.
Enter negative required height for geosynchronous altitude.

Enter initial perigee height (km): 400
Enter initial apogee height (km): 65000
Enter required inclination change (°): 12.5
Enter required perigee height (km): -1
Geosynchronous perigee = 35786.0 km
Enter required apogee height (km): -1
Geosynchronous apogee = 35786.0 km

Burn at 65000.0 km: theta1 = 11.74°, dv1 = 1091.4 m/s
Burn at 35786.0 km: theta2 =  0.76°, dv2 =  375.5 m/s
dv = 1466.9 m/s
Saved 2.6 m/s


Thanks.
Liftoff for St. Jude's! Go Dragon, Go Falcon, Godspeed Inspiration4!

Offline FutureSpaceTourist

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Offline Steven Pietrobon

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They showed the Falcon Heavy Viasat launch at ignition!
Akin's Laws of Spacecraft Design #1:  Engineering is done with numbers.  Analysis without numbers is only an opinion.

Online Galactic Penguin SST

They showed the Falcon Heavy Viasat launch at ignition!
Their first satellite Arcturus was on board this launch as a hitchhiker so at least it was somewhat relevant.
Astronomy & spaceflight geek penguin. In a relationship w/ Space Shuttle Discovery.

Offline gongora

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62454   OBJECT A   2024-252A   12.31   64611   353
62455   OBJECT B   2024-252B   12.38   64612   327
62456   OBJECT C   2024-252C   12.43   64467   390
62457   OBJECT D   2024-252D   12.36   64527   340
62458   FALCON 9 R/B   2024-252E   12.41   63485   219

Offline FutureSpaceTourist

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https://twitter.com/pronounced_kyle/status/1877524191827865759

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THOSE LITTLE DOTS ARE OUR SATELLITES. IN SPACE.

(Thank you to @s2a_systems for spotting them!)

Offline FutureSpaceTourist

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https://twitter.com/gedmark/status/1877807285562683800

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Huge update from Astranis Mission Control: all four Block 2 satellites have successfully completed initial commissioning and are now headed to GEO using their on board ion thrusters.

This is a huge deal. Here are some highlights from our first week and half on orbit:

- Nominal deployment in our target orbit: 400km x 65,000km x 12.5 deg inclination (thank you SpaceX)
- All pre-separation logic and separation autonomy worked perfectly, and all autonomous deployments (solar arrays, ion thruster gimbals, and secondary antenna reflectors) successfully completed
- Checkouts of thermal management systems, power subsystems, software, and GNC
- Reaction wheel, SADA, and monopropellant thruster commissioning
- Monoprop detumble and transition to fine pointing control using reaction wheels and star trackers
- Sun-pointing mode achieved for maximum power generation
- High rate TTC downlink and download of onboard data
- Subreflector boom deployment and verification via photodiode telemetry
- Ion thruster gimbal commissioning, demonstrating successful gimbal deployment
- Simultaneous command of all 5 Astranis satellites, using 9 different ground stations across 4 continents
- 100% successful deployments: all solar arrays, booms, gimbals, reflectors, splashplates — 60x total hold down release mechanism deployments without issue
- Test-fired and characterized all 8 monoprop thrusters on all 4 satellites (32x thrusters total)
- Commissioned the Electric Propulsion (EP) system, including successfully test-firing each satellite's ion thruster
- Conducted an initial payload checkout on all 4 vehicles— the Software-Defined Radios, RF front end electronics, high-power amplifiers (TWTAs), and LNAs have all been checked out and are performing nominally
- Executed long-duration EP burns on all four vehicles, and have beginning orbit raises to GEO from our current GTO orbits

In short: the satellites are working great and are on their way to GEO where they will start their missions for our customers. All of our hard work — designing, testing, manufacturing, and operating — is paying off.

LET’S GO.

Offline StraumliBlight

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Our new satellites have now been on orbit for an entire month!

This footage is incredibly unique — four GEO-bound satellites, captured immediately after deployment, and near perigee, from space. We hope you enjoy it as much as we did.

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