Author Topic: SpaceX F9 : SES-10 with reuse of CRS-8 Booster SN/1021 : 2017-03-30 : DISCUSSION  (Read 510369 times)

Offline mme

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I'm a fan of SpaceX, I think they will succeed and I believe they have done all their homework for this flight.

But claiming "no biggie, it's insured" for the customer does not recognize that satellites take years to build and companies like SES, Iridium, Orbcomm, and dare I mention Spacecom make their livelihood by those satellites being operational in orbit.

My house is insured but if it burns down it's still going to suck. If I ever meet the CTO of SES, I'm buying the man a drink for supporting SpaceX and reusable rockets. Even though I am sure he got a sweet deal for this flight.
Space is not Highlander.  There can, and will, be more than one.

Offline rsdavis9

Has anybody considered the PR that companies like SES get for being the first to launch on a new spacex configuration. I know that personally I know a lot more about SES now then before their flights. I think Iridium got a boost from the PR too.
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 rockets4life97

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Any reason for the longer burn? Special request by SES?

Does it result in better data being collected (vs a 3 second burn)? If yes, why not make 5 second burns standard?

I think I remember someone saying the 5 sec burn allows them to get a better checkout of the turbopumps.
« Last Edit: 03/27/2017 06:19 pm by rockets4life97 »

Offline Lar

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Any reason for the longer burn? Special request by SES?

Does it result in better data being collected (vs a 3 second burn)? If yes, why not make 5 second burns standard?

I think I remember someone saying the 5 sec burn allows them to get a better checkout of the turbopumps.

Which does kind of revalidate the question... why not do this for all? I honestly have no idea. Might be off topic for a mission specific thread. Maybe we need a "how long to static fire" thread! :) Or a poll.  (KIDDING)
"I think it would be great to be born on Earth and to die on Mars. Just hopefully not at the point of impact." -Elon Musk
"We're a little bit like the dog who caught the bus" - Musk after CRS-8 S1 successfully landed on ASDS OCISLY

Offline ChrisGebhardt

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Any reason for the longer burn? Special request by SES?

Does it result in better data being collected (vs a 3 second burn)? If yes, why not make 5 second burns standard?

I think I remember someone saying the 5 sec burn allows them to get a better checkout of the turbopumps.

Which does kind of revalidate the question... why not do this for all? I honestly have no idea. Might be off topic for a mission specific thread. Maybe we need a "how long to static fire" thread! :) Or a poll.  (KIDDING)

As they've only done (to my memory) the prolonged static fire for the two SES missions to date, I'd place good money on it being a customer request.

Offline rsdavis9

Any reason for the longer burn? Special request by SES?

Does it result in better data being collected (vs a 3 second burn)? If yes, why not make 5 second burns standard?

I think I remember someone saying the 5 sec burn allows them to get a better checkout of the turbopumps.

Which does kind of revalidate the question... why not do this for all? I honestly have no idea. Might be off topic for a mission specific thread. Maybe we need a "how long to static fire" thread! :) Or a poll.  (KIDDING)

As they've only done (to my memory) the prolonged static fire for the two SES missions to date, I'd place good money on it being a customer request.

So whats the TEL umbilical damage like for A static fire? Does the longer burn do more damage?
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 kevinof

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I assume none as it never contacts the exhaust.  It's only (?) as the stage climbs off the pad that the heat and exhaust impacts the tel and causes damage.

Any reason for the longer burn? Special request by SES?

Does it result in better data being collected (vs a 3 second burn)? If yes, why not make 5 second burns standard?

I think I remember someone saying the 5 sec burn allows them to get a better checkout of the turbopumps.

Which does kind of revalidate the question... why not do this for all? I honestly have no idea. Might be off topic for a mission specific thread. Maybe we need a "how long to static fire" thread! :) Or a poll.  (KIDDING)

As they've only done (to my memory) the prolonged static fire for the two SES missions to date, I'd place good money on it being a customer request.

So whats the TEL umbilical damage like for A static fire? Does the longer burn do more damage?
« Last Edit: 03/27/2017 06:54 pm by kevinof »

Offline ChrisGebhardt

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I assume none as it never contacts the exhaust.  It's only (?) as the stage climbs off the pad that the heat and exhaust impacts the tel and causes damage.

Any reason for the longer burn? Special request by SES?

Does it result in better data being collected (vs a 3 second burn)? If yes, why not make 5 second burns standard?


I think I remember someone saying the 5 sec burn allows them to get a better checkout of the turbopumps.

Which does kind of revalidate the question... why not do this for all? I honestly have no idea. Might be off topic for a mission specific thread. Maybe we need a "how long to static fire" thread! :) Or a poll.  (KIDDING)

As they've only done (to my memory) the prolonged static fire for the two SES missions to date, I'd place good money on it being a customer request.

So whats the TEL umbilical damage like for A static fire? Does the longer burn do more damage?

Correct.  No TEL umbilical damage from a nominal static fire.
« Last Edit: 03/27/2017 06:55 pm by ChrisGebhardt »

Offline ugordan

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As they've only done (to my memory) the prolonged static fire for the two SES missions to date, I'd place good money on it being a customer request.

+ Jason-3

Offline THeel01

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Can someone double check my math?
By my count, the current record for pad turnaround for launches on either LC39A/B is 17 days (STS- 51-D to STS-51-B, launched from LC39A).
Not to start Go-fever or anything, but if SpaceX launches on Mar 30, thats 14 day turnaround.
Sound correct?

Offline Mike_1179

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As they've only done (to my memory) the prolonged static fire for the two SES missions to date, I'd place good money on it being a customer request.

If this static fire is meant to mimic the ignition and hold down of a real launch, does that mean they intend to hold the vehicle down for 5 seconds after ignition on the 30th as well?

The downside is 2 seconds less prop at the end of a first stage burn but my guess is it lets them characterize the engine performance prior to hold-down release better once you get further away from start-up transients and they operate at steady state. Might be that's why this is a "customer request" because the customer is getting 2 seconds less margin (about 500 kg of fuel, right?)

Offline ChrisGebhardt

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As they've only done (to my memory) the prolonged static fire for the two SES missions to date, I'd place good money on it being a customer request.

If this static fire is meant to mimic the ignition and hold down of a real launch, does that mean they intend to hold the vehicle down for 5 seconds after ignition on the 30th as well?

The downside is 2 seconds less prop at the end of a first stage burn but my guess is it lets them characterize the engine performance prior to hold-down release better once you get further away from start-up transients and they operate at steady state. Might be that's why this is a "customer request" because the customer is getting 2 seconds less margin (about 500 kg of fuel, right?)

No.  Sequence on launch day will result in nominal release time at T0.

Offline Orbiter

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Can someone double check my math?
By my count, the current record for pad turnaround for launches on either LC39A/B is 17 days (STS- 51-D to STS-51-B, launched from LC39A).
Not to start Go-fever or anything, but if SpaceX launches on Mar 30, thats 14 day turnaround.
Sound correct?

Yes, assuming the schedule holds, the turnaround between Echostar-23 and SES-10 will be the fastest ever from LC-39A. However, the Shuttle was a far different beast.
« Last Edit: 03/27/2017 08:12 pm by Orbiter »
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Offline ATPTourFan

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No.  Sequence on launch day will result in nominal release time at T0.

I would agree, clamps release at T-0, but would ignition sequence start earlier?

It's a good question because I thought the "only" thing different between static hold-down fire pre-launch was that they didn't let go (I know that's oversimplified). Or is the static fire a modified sequence that only mimics the pad operations and fuel loading profile for the launch through to engine ignition, and not necessarily a mirror of the last 5 seconds prior to T-0?
« Last Edit: 03/27/2017 08:55 pm by ATPTourFan »

Offline ChrisGebhardt

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No.  Sequence on launch day will result in nominal release time at T0.

I would agree, clamps release at T-0, but would ignition sequence start earlier?

It's a good question because I thought the "only" thing different between static hold-down fire pre-launch was that they didn't let go (I know that's oversimplified). Or is the static fire a modified sequence that only mimics the pad operations and fuel loading profile for the launch through to engine ignition, and not necessarily a mirror of the last 5 seconds prior to T-0?

No.  The countdown sequence will be nominal.  No extra time or early ignition, etc..  The static fire duration does not translate to changes to launch countdown.

Static fire is a mirror of everything down to T0.  If it helps, a good way to think of today is that they proceeded past T0 to T+2secs, but didn't release the clamps.  That's a better way to view this than a change to countdown/launch day/release timing.
« Last Edit: 03/27/2017 09:18 pm by ChrisGebhardt »

Offline mn

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How many seconds between ignition and T0?

Is this time consistent or has anyone noticed that number moving around on various launches?

Offline ugordan

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Chamber ignition occurs at around T-2 sec with TEA/TEB starting flowing about a second before that. Has been that way for IIRC as long as M1D existed.

Offline ChrisC

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Offline intrepidpursuit

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How many seconds between ignition and T0?

See background here:  https://www.google.com/search?q=Falcon+9+ignition+sequence

That is a useless link. None of the first page results provide any meaningful insight into the Merlin startup sequence.

Offline DatUser14

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How many seconds between ignition and T0?

Is this time consistent or has anyone noticed that number moving around on various launches?
Looked at the last couple press kits, it's been T-3 Merlin-1D ignition T-0 liftoff.
Titan IVB was a cool rocket

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