Author Topic: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD  (Read 611306 times)

Offline Roy_H

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #900 on: 12/03/2013 10:08 pm »
I am presuming that the relight will come as the stage and payload pass over the Equator.

As I understand it, they are aiming for an orbit with a 19 degree inclination, so I would expect the relight to happen earlier.
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Offline Roy_H

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #901 on: 12/03/2013 10:13 pm »
Relight successful!
"If we don't achieve re-usability, I will consider SpaceX to be a failure." - Elon Musk
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Offline Lars_J

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #902 on: 12/03/2013 10:14 pm »
I am presuming that the relight will come as the stage and payload pass over the Equator.

As I understand it, they are aiming for an orbit with a 19 degree inclination, so I would expect the relight to happen earlier.

No, the most efficient place for the combined burn to raise apogee and change inclination is at the equator. And they care more about the location of the apogee than they do about the specific inclination.

And Elon tweeted: https://twitter.com/elonmusk/status/408008759433502720
Quote
Elon Musk ‏@elonmusk
Reached parking orbit. Now coasting towards equator, where the upper stage will, if all goes well, restart to raise apogee
« Last Edit: 12/03/2013 10:16 pm by Lars_J »

Offline IRobot

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #903 on: 12/03/2013 10:21 pm »
What happens to the 2nd stage now? trails behind SES forever or does a 3rd burn to reenter?

Offline jongoff

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #904 on: 12/03/2013 10:22 pm »
Did separation actually get confirmed? Someone said it was confirmed here, but I didn't actually see a post saying that...

~Jon

Offline jongoff

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #905 on: 12/03/2013 10:22 pm »
And of course just after saying that:
SpaceX ‏@SpaceX 9s

Spacecraft separation confirmed! SES-8 is now in its targeted GEO transfer orbit.

Offline Lars_J

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #906 on: 12/03/2013 10:23 pm »
What happens to the 2nd stage now? trails behind SES forever or does a 3rd burn to reenter?

I think it will trail behind for now (until SES-8 does its apogee burn) and with its low perigee it should reenter at some point in the not too distant future. (not sure how many orbits, but it should be a lot)

Offline QuantumG

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #907 on: 12/03/2013 10:23 pm »
What happens to the 2nd stage now? trails behind SES forever or does a 3rd burn to reenter?

I don't believe they intend to deliberately deorbit it.

What's the perigee? Should be able to figure out when it'll eventually come down.
Human spaceflight is basically just LARPing now.

Offline Helodriver

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #908 on: 12/03/2013 10:24 pm »
With the very visible 1st stage RCS firings after staging, I hope they got some good data and practice controlling the stage orientation for future landings. I wonder if what they did will be addressed post launch sometime?

Offline jongoff

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #909 on: 12/03/2013 10:24 pm »
Peter B. de Selding ‏@pbdes 12s

SES has acquired spacecraft and it is in good health.

Offline IRobot

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #910 on: 12/03/2013 10:26 pm »
What happens to the 2nd stage now? trails behind SES forever or does a 3rd burn to reenter?

I don't believe they intend to deliberately deorbit it.

What's the perigee? Should be able to figure out when it'll eventually come down.
A 3rd restart would prove multiple restart capability. They will need it eventually.

Offline bioelectromechanic

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #911 on: 12/03/2013 10:28 pm »
Is there a post launch conference planned? when?
Carpe diem et vadem ad astra

Offline QuantumG

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #912 on: 12/03/2013 10:37 pm »
I'm under the impression that to execute a mission like this while recovering the first stage, a Falcon Heavy would be necessary, right ?

Nope. SpaceX can fly a GTO mission on Falcon 9 v1.1 and recover the first stage. They didn't on this flight because it was their first and they wanted to dedicate as much margin as possible to the flight trajectory.
Human spaceflight is basically just LARPing now.

Offline Robotbeat

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #913 on: 12/03/2013 10:39 pm »
I'm under the impression that to execute a mission like this while recovering the first stage, a Falcon Heavy would be necessary, right ?
No, F9R is enough. SpaceX just did not want to risk it and gave full 1st stage performance.
Are you sure? You may be right, but I'd like some sort of confirmation. Some GTO missions might not provide enough performance to do a RTLS. It could be they might be able to recover stages from the ocean as an intermediate step, but I'm not even sure that's feasible here.

In any case, a higher energy upper stage would allow first stage recovery even with big GTO payloads.
« Last Edit: 12/03/2013 10:43 pm by Robotbeat »
Chris  Whoever loves correction loves knowledge, but he who hates reproof is stupid.

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Offline butters

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #914 on: 12/03/2013 10:40 pm »
Now they'd want to get a handle on how much residual prop they have in the upper stage, to refine their performance margins.

Offline Lars_J

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #915 on: 12/03/2013 10:41 pm »
A cool view of the launch:

I wonder, is this after MVac ignition, or is it all first stage?

Offline IRobot

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #916 on: 12/03/2013 10:43 pm »
I'm under the impression that to execute a mission like this while recovering the first stage, a Falcon Heavy would be necessary, right ?
No, F9R is enough. SpaceX just did not want to risk it and gave full 1st stage performance.
Are you sure? You may be right, but I'd like some sort of confirmation. Some GTO missions might not provide enough performance to do a RTLS. It could be they might be able to recover stages from the ocean as an intermediate step, but I'm not even sure that's feasible here.

That is what I understand from this:

Quote
Musk indicated that SpaceX would not attempt to recover the first stage for the SES and Thaicom flights, instead “(for) the next two launches, we are going to gather data from the first stage but we are not going to attempt to recover it because we’ve committed to give the customers on the next two flights maximum performance of the rocket. The next recovery attempt for the first stage will be the fourth flight of this version.”

http://www.nasaspaceflight.com/2013/10/ses-8-florida-next-falcon-9-v1-1-launch/

EDIT: and here http://forum.nasaspaceflight.com/index.php?topic=24469.465
« Last Edit: 12/03/2013 10:45 pm by IRobot »

Offline Lars_J

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #917 on: 12/03/2013 10:48 pm »
If anyone missed it on the update thread, here is a Youtube replay of the launch:
(And at 3:20 we get a very clear view of the first stage RCS firing)



I've attached an image... The blue exhaust is definitely the RCS, the white may just be M1D or tank venting:
« Last Edit: 12/03/2013 10:52 pm by Lars_J »

Offline Herb Schaltegger

Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #918 on: 12/03/2013 10:48 pm »
I'm under the impression that to execute a mission like this while recovering the first stage, a Falcon Heavy would be necessary, right ?
No, F9R is enough. SpaceX just did not want to risk it and gave full 1st stage performance.
Are you sure? You may be right, but I'd like some sort of confirmation. Some GTO missions might not provide enough performance to do a RTLS. It could be they might be able to recover stages from the ocean as an intermediate step, but I'm not even sure that's feasible here.

Indeed. The most recently-flown Directv satellites were Boeing 702's. Each massed over 6,000 kg at launch, almost twice the mass of SES-8. That is well above Falcon 9's stated payload to GTO of 4,850 kg.
« Last Edit: 12/03/2013 10:49 pm by Herb Schaltegger »
Ad astra per aspirin ...

Offline QuantumG

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Re: SpaceX Falcon 9 v1.1 - SES-8 - DISCUSSION THREAD
« Reply #919 on: 12/03/2013 10:49 pm »
and also:

Quote from: Elon Musk
The next two flights are somewhat of an exception. When we negotiated these deals, we didn't have much bargaining power. It was before we obviously flown this version of the Falcon 9 successfully. So we kind of agreed to give up all performance on the rocket and not reserve anything for reusability. But going into the future, with future contracts, with a few exceptions, we have reserved enough performance to recover the stage.

http://shitelonsays.com/transcript/spacex-press-conference-september-29-2013-2013-09-29
Human spaceflight is basically just LARPing now.

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