Author Topic: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD  (Read 271806 times)

Offline Norm38

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #300 on: 01/06/2014 01:57 pm »
NWS is forecasting wind gusts of 25-30mph for the Cape this afternoon.  Anyone know what the limit is for launch?

Offline Thunderbird5

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #301 on: 01/06/2014 02:09 pm »
Here is official Patrick's weather forecast: http://www.patrick.af.mil/shared/media/document/AFD-070716-028.pdf

Those wind speeds look slightly concerning, although I note the combined wind/cloud violation is still only 20%. Do we know what the upper launch thresholds are for wind speed of the F9 v1.1?

Edit: typo
« Last Edit: 01/06/2014 02:12 pm by Thunderbird5 »

Offline edkyle99

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #302 on: 01/06/2014 02:09 pm »
Only 3016 kg. I thought it was higher.

Anyway orbit is going to 295x90,000x22.5
90,000 kilometers at apogee? Is this correct? AIUI SES-8 went to Super Synchronous Orbit but Thaicom-6 was going to a standard GSO. If it's going up to 90,000 kilometers, is it going to a Super Synchronous Orbit too?

There is that discrepancy in the press kit. They write GTO and then give these data, which is SSTO.

A super synchronous transfer orbit is used as a type of geosynchronous transfer orbit, so no discrepancy. 

Atlas Centaurs sent satellites to supersync orbits with apogees as high as 130,000 km during the 1990s, so this is nothing new, although 90,000 km is higher than most.

 - Ed Kyle
« Last Edit: 01/06/2014 02:28 pm by edkyle99 »

Offline TrueBlueWitt

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #303 on: 01/06/2014 02:22 pm »
Is there confirmation that LV is erect on the pad? This is quietest start to a launch day I can remember

Offline andrewsdanj

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #304 on: 01/06/2014 02:32 pm »
Spaceflight Now's Facebook page has a photograph of the vehicle vertical, partly obscured by fog.

"It's a foggy morning at the pad as SpaceX readies the Falcon 9 rocket for launch today at Cape Canaveral."

https://www.facebook.com/photo.php?fbid=592826850786718&set=a.131474330255308.25052.123621931040548&type=1&theater

Edit: SpaceX's Facebook updated 15:36Z with a photo of the vehicle vertical minus fog.
« Last Edit: 01/06/2014 02:40 pm by andrewsdanj »

Offline JBF

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #305 on: 01/06/2014 02:36 pm »
So SpaceX posted a picture from this morning, is fog a typical occurrence this time of year and does it usually burn off?
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Offline Comga

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #306 on: 01/06/2014 03:08 pm »
Only 3016 kg. I thought it was higher.

Anyway orbit is going to 295x90,000x22.5
That is a very high SSTO. :)

SSTO is already in the acronym list for something other than Supra-Syncronous Transfer Orbit. ;)
What kind of wastrels would dump a perfectly good booster in the ocean after just one use?

Offline edkyle99

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #307 on: 01/06/2014 03:21 pm »
So SpaceX posted a picture from this morning, is fog a typical occurrence this time of year and does it usually burn off?
My recollection is that fog is more likely during the winter months in that area, but it does usually burn off.  The weather issue today is wind and the approaching "Arctic Vortex" cold front that will bring temperatures down to near freezing tonight.  I weep for those Floridians from my position right now in Illinois, days of snow piled high, where it is 14 below zero Fahrenheit (-40 something with wind chill).

 - Ed Kyle
« Last Edit: 01/06/2014 03:25 pm by edkyle99 »

Offline Chris Bergin

Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #308 on: 01/06/2014 03:23 pm »
So SpaceX posted a picture from this morning, is fog a typical occurrence this time of year and does it usually burn off?

Ironically, the F9 v1.1 has shown a habit for creating her own fog during tanking.....although I think that has a lot to do with humidity during SES-8. Biggest venter I've seen.
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Offline Antares

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #309 on: 01/06/2014 04:22 pm »
I wonder how SpaceX is characterizing the onboard fuel temperature today.  There will be a significant thermal transient during loading as the arctic vortex reaches Florida.  The temperature coming out of the storage tanks will not be what lifts off.
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Offline Lar

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #310 on: 01/06/2014 04:24 pm »
From the press kit: (link given above)

Quote
An upgraded Falcon 9 with safety and reliability enhancements and greater
lift capability flew for the first time in December 2013, lofting the SES-8
satellite to a geosynchronous transfer orbit , and will fly on this mission.

I was surprised to see that wording since the first v 1.1 was CASSIOPE... are they trying to introduce a second dot in their versioning, so CASSIOPE is 1.1 and SES-8 is 1.1.1 ???  Or is that a typo?
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Offline AS-503

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #311 on: 01/06/2014 04:35 pm »
From the press kit: (link given above)

Quote
An upgraded Falcon 9 with safety and reliability enhancements and greater
lift capability flew for the first time in December 2013, lofting the SES-8
satellite to a geosynchronous transfer orbit , and will fly on this mission.

I was surprised to see that wording since the first v 1.1 was CASSIOPE... are they trying to introduce a second dot in their versioning, so CASSIOPE is 1.1 and SES-8 is 1.1.1 ???  Or is that a typo?


I saw that too. I think they are referring to the second stage re-light fix employed after Cassiope. There are probably other things they learned from that first V1.1 flight that prompted some modifications as well.

Offline Lar

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #312 on: 01/06/2014 04:38 pm »
From the press kit: (link given above)

Quote
An upgraded Falcon 9 with safety and reliability enhancements and greater
lift capability flew for the first time in December 2013, lofting the SES-8
satellite to a geosynchronous transfer orbit , and will fly on this mission.

I was surprised to see that wording since the first v 1.1 was CASSIOPE... are they trying to introduce a second dot in their versioning, so CASSIOPE is 1.1 and SES-8 is 1.1.1 ???  Or is that a typo?


I saw that too. I think they are referring to the second stage re-light fix employed after Cassiope. There are probably other things they learned from that first V1.1 flight that prompted some modifications as well.

Nod. I just would have expected them to talk more about the v 1.0 to 1.1 and less about the post CASSIOPE fixes :) 

Many posters have remarked that today, every rocket will have changes from the last one, every time.   Of course SpaceX will want that not to be the case, introducing changes in batches (as vehicle manufacturers or electronics manufacturers do) for cost reasons.
« Last Edit: 01/06/2014 04:40 pm by Lar »
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Offline Hauerg

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #313 on: 01/06/2014 04:50 pm »
The first burn of the second stage is going to be 335 seconds. The duration of the second burn is unknown.  :-X

Almost true:
"...the second stage will relight for just over one minute"  Presskit, p.4

Offline Comga

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #314 on: 01/06/2014 05:19 pm »
Looking at the photo linked in this post does anyone think that SpaceX intentionally obsucrred the base of the rocket by takinig the photo where it is just behind the flame trench opening?
What kind of wastrels would dump a perfectly good booster in the ocean after just one use?

Offline ChrisWilson68

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #315 on: 01/06/2014 05:22 pm »
Looking at the photo linked in this post does anyone think that SpaceX intentionally obsucrred the base of the rocket by takinig the photo where it is just behind the flame trench opening?

I have to admit that thought occurred to me too.  That particular angle makes it impossible to see if there are legs attached.

Offline newpylong

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #316 on: 01/06/2014 05:29 pm »
No legs.

Offline Comga

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #317 on: 01/06/2014 05:29 pm »
Looking at the photo linked in this post does anyone think that SpaceX intentionally obsucrred the base of the rocket by takinig the photo where it is just behind the flame trench opening?

I have to admit that thought occurred to me too.  That particular angle makes it impossible to see if there are legs attached.

We have no reason to suspect that there are legs, as their presence on the CRS-3 rocket are still uncertain.
Adding legs would go against the statement of maximizing performance and replicating the SES-8 launch. 

edit: newpylong: Is that a statement of fact from observation, a second hand report from a good source, or your supposition (with which my statement above concurrs)?
« Last Edit: 01/06/2014 05:31 pm by Comga »
What kind of wastrels would dump a perfectly good booster in the ocean after just one use?

Offline Borklund

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Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #318 on: 01/06/2014 05:30 pm »
You've gone a little too far with the Kremlinology this time chaps.

Offline MP99

Re: SpaceX Falcon 9 v1.1 - Thaicom 6 - DISCUSSION THREAD
« Reply #319 on: 01/06/2014 05:35 pm »
From the press kit: (link given above)

Quote
An upgraded Falcon 9 with safety and reliability enhancements and greater
lift capability flew for the first time in December 2013, lofting the SES-8
satellite to a geosynchronous transfer orbit , and will fly on this mission.

I was surprised to see that wording since the first v 1.1 was CASSIOPE... are they trying to introduce a second dot in their versioning, so CASSIOPE is 1.1 and SES-8 is 1.1.1 ???  Or is that a typo?


I saw that too. I think they are referring to the second stage re-light fix employed after Cassiope. There are probably other things they learned from that first V1.1 flight that prompted some modifications as well.

SES-8 was first from the Cape, but still surprising to see this listed as second of what sounds like v1.1, rather than third.

cheers, Martin

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