Author Topic: SpaceX F9 : Crew Dragon In-Flight Abort Test : Jan. 19, 2020 : Discussion  (Read 366119 times)

Offline whitelancer64

Max drag is the most difficult in-flight regime in which to abort, your opinion not withstanding.

Okay, but why exactly?  MaxQ is max drag.  After separation the streamlined Dragon will have less aero drag than the uncapped F9.  Wouldn't that increase the acceleration difference between the two?  And if any debris was thrown out by F9 disintegrating, that debris will also have max drag and be much less likely to catch up to Dragon.

I just want to understand better exactly why MaxQ is worst case when the forces seem to be working against it.

The abort test has nothing to do with the rocket. Let's make that super clear. So, what the rocket does after separation doesn't matter. That's why you can perform an abort test using a different rocket.

What's being tested is the abort system itself. So the best test (or the "worst case scenario") is when the abort system would have to work the hardest to separate the capsule from the rocket. That's when aerodynamic drag peaks, right around Max Q.
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Offline meberbs

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If the S1 engines are shut down prior to abort, relative acceleration isn't minimum.  At MaxQ, S1 thrusting acceleration is not yet maximum.  And with MaxQ having maximum drag, the F9 will have maximum deceleration following separation.

The drag would primarily be on Dragon, not the F9, just like race cars drift close  behind each other so that only the lead car needs to fully deal with drag. For the crucial first instant of separation, this difference in drag should be one version worst case.

Plus if the shutdown command to the engine happens at the same time as startup of the abort thrusters, the Merlins will still be in shutdown transient at that time, while simultaneously having less mass to accelerate as dragon detaches, and less drag to deal with, since most of it is on the capsule.

Offline woods170

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If the Falcon 9 booster breaks up in flight, then it won't meet all of the desired test criteria (i.e. the capsule won't experience the dynamic pressure it was supposed to). It would mean, most likely, another in-flight abort test, at great cost and a big schedule delay for SpaceX.
Disagree.  It would mean, more likely, that SpaceX would apply the findings to their simulation and just simulate the max-q abort, as Boeing is doing (without any flight data of the stack with the capsule at all).  Depending on how close it got to max-q, if it blows up early in the flight it would generate little valuable data in that regard.

Of course, it would also mean that SpaceX experienced an unexpected Falcon 9 failure that would need to be root-cause analyzed and set the progress of the program way back, frankly more than conducting another in-flight abort would likely result in on its own.  Little Joe failing on its own had no implication on the Apollo stack.

Emphasis mine.

Yes, this.

People here have to remember that none of the abort flight-tests were required by NASA. Under the CCiCAP and CCtCAP contracts NASA only required the CCP contractors to model the abort regime, along with extensive ground-testing of the abort motors.
Boeing added a pad-abort flight test as a voluntary milestone to its CCtCAP contract.
SpaceX added both a pad-abort flight test and a Max-Q ascent abort test as voluntary milestones to its CCiCAP contract.

If any of those tests fail the CCP contractor in question will revert back to the default NASA requirment: modeling only of the abort regimes. No repeat or reflights of failed abort test flights.

Offline Semmel

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If the Falcon 9 booster breaks up in flight, then it won't meet all of the desired test criteria (i.e. the capsule won't experience the dynamic pressure it was supposed to). It would mean, most likely, another in-flight abort test, at great cost and a big schedule delay for SpaceX.
Disagree.  It would mean, more likely, that SpaceX would apply the findings to their simulation and just simulate the max-q abort, as Boeing is doing (without any flight data of the stack with the capsule at all).  Depending on how close it got to max-q, if it blows up early in the flight it would generate little valuable data in that regard.

Of course, it would also mean that SpaceX experienced an unexpected Falcon 9 failure that would need to be root-cause analyzed and set the progress of the program way back, frankly more than conducting another in-flight abort would likely result in on its own.  Little Joe failing on its own had no implication on the Apollo stack.

Emphasis mine.

Yes, this.

People here have to remember that none of the abort flight-tests were required by NASA. Under the CCiCAP and CCtCAP contracts NASA only required the CCP contractors to model the abort regime, along with extensive ground-testing of the abort motors.
Boeing added a pad-abort flight test as a voluntary milestone to its CCtCAP contract.
SpaceX added both a pad-abort flight test and a Max-Q ascent abort test as voluntary milestones to its CCiCAP contract.

If any of those tests fail the CCP contractor in question will revert back to the default NASA requirment: modeling only of the abort regimes. No repeat or reflights of failed abort test flights.

But both get payed for the voluntary milestones, right? So if the test fails, no milestone money. I guess doing the abort tests was a financial decision for both companies, not the need for information necessarily. Its good to have the real world data, but if simulations are fine for NASA, its hard to believe that SpaceX or ULA wouldnt be fine with that as well. So I guess SpaceX just thinks they can make a profit from the inflight abort test and that is the primary motivation for doing it.

Online abaddon

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They were not required but they were encouraged and part of the bid selection process overall.  Suggesting SpaceX wants to do this strictly for financial reasons is absurd.

Online gongora

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But both get payed for the voluntary milestones, right? So if the test fails, no milestone money. I guess doing the abort tests was a financial decision for both companies, not the need for information necessarily. Its good to have the real world data, but if simulations are fine for NASA, its hard to believe that SpaceX or ULA wouldnt be fine with that as well. So I guess SpaceX just thinks they can make a profit from the inflight abort test and that is the primary motivation for doing it.

Unless the payment has increased a lot from the last time we saw those contract numbers, it's not likely SpaceX could make money on the abort test even with a reused booster.  It's also not likely that much (maybe not any) of the payment would be tied to the complete success of the test.

Offline soltasto

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But both get payed for the voluntary milestones, right? So if the test fails, no milestone money. I guess doing the abort tests was a financial decision for both companies, not the need for information necessarily. Its good to have the real world data, but if simulations are fine for NASA, its hard to believe that SpaceX or ULA wouldnt be fine with that as well. So I guess SpaceX just thinks they can make a profit from the inflight abort test and that is the primary motivation for doing it.

Unless the payment has increased a lot from the last time we saw those contract numbers, it's not likely SpaceX could make money on the abort test even with a reused booster.  It's also not likely that much (maybe not any) of the payment would be tied to the complete success of the test.

Yeah, it should only be $30 Million.

Offline ChrisC

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Is it time to split this thread into updates vs discussion?
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Offline ZachS09

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Is it time to split this thread into updates vs discussion?

I think it's a good idea.
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Online gongora

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Is it time to split this thread into updates vs discussion?

It's probably still a bit early for that.

Offline rcoppola

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The update clock starts the moment DM-1 splashes down and is sent back to Hawthorne for refurb. That's the pacing item. More so than the F9 that they already sent back to the barn.
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Offline whitelancer64

If the Falcon 9 booster breaks up in flight, then it won't meet all of the desired test criteria (i.e. the capsule won't experience the dynamic pressure it was supposed to). It would mean, most likely, another in-flight abort test, at great cost and a big schedule delay for SpaceX.
Disagree.  It would mean, more likely, that SpaceX would apply the findings to their simulation and just simulate the max-q abort, as Boeing is doing (without any flight data of the stack with the capsule at all).  Depending on how close it got to max-q, if it blows up early in the flight it would generate little valuable data in that regard.

Of course, it would also mean that SpaceX experienced an unexpected Falcon 9 failure that would need to be root-cause analyzed and set the progress of the program way back, frankly more than conducting another in-flight abort would likely result in on its own.  Little Joe failing on its own had no implication on the Apollo stack.

Emphasis mine.

Yes, this.

People here have to remember that none of the abort flight-tests were required by NASA. Under the CCiCAP and CCtCAP contracts NASA only required the CCP contractors to model the abort regime, along with extensive ground-testing of the abort motors.
Boeing added a pad-abort flight test as a voluntary milestone to its CCtCAP contract.
SpaceX added both a pad-abort flight test and a Max-Q ascent abort test as voluntary milestones to its CCiCAP contract.

If any of those tests fail the CCP contractor in question will revert back to the default NASA requirment: modeling only of the abort regimes. No repeat or reflights of failed abort test flights.

The self-imposed milestones are still required milestones. They are not "voluntary" such that they could decide to skip them, they are "mandatory" in that respect.  AIUI, they are contractually obligated to complete them to NASA's satisfaction.
« Last Edit: 02/28/2019 03:00 pm by whitelancer64 »
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"There are lies, damned lies, and launch schedules." - Larry J

Online FutureSpaceTourist

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At the NASA social briefing just now for DM-1, Benji Reed from SpaceX (Director of Crew Management) was asked about the in-flight abort test. He said that SpaceX would ideally like to bring the booster home. So maybe they'll equip it for a return (although as Elon recent said it may well not survive).

The update clock starts the moment DM-1 splashes down and is sent back to Hawthorne for refurb. That's the pacing item. More so than the F9 that they already sent back to the barn.

Are you sure it's being sent back to Hawthorne for the refurb? I thought I saw something that indicated for the Iin-Flight Abort test, that the Crew Dragon would stay at the Cape for all In-Flight Abort test preparations.

Offline cppetrie

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What is the status of the Dragon processing facility they were building at LZ1? If it is staying at the cape, which makes sense if they want to turn it around relatively quickly, then that is presumably where the work would be done.

Offline rcoppola

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The update clock starts the moment DM-1 splashes down and is sent back to Hawthorne for refurb. That's the pacing item. More so than the F9 that they already sent back to the barn.

Are you sure it's being sent back to Hawthorne for the refurb? I thought I saw something that indicated for the Iin-Flight Abort test, that the Crew Dragon would stay at the Cape for all In-Flight Abort test preparations.
I have not heard anyone at SpaceX confirm where refurb will take place. Perhaps that will be asked over the next few Press-conferences. My thinking for sending back to Hawthorne is just that its the first of its kind and all the designers, engineers, machinery and tools needed for evaluation, mods, replacements, etc. are in Hawthorne. I think it's too early in the program for a major Dragon2 evaluation and refurb to be done anywhere but Hawthorne. But I could be wrong for sure.
« Last Edit: 02/28/2019 04:49 pm by rcoppola »
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Offline RocketLover0119

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At the NASA social briefing just now for DM-1, Benji Reed from SpaceX (Director of Crew Management) was asked about the in-flight abort test. He said that SpaceX would ideally like to bring the booster home. So maybe they'll equip it for a return (although as Elon recent said it may well not survive).

They were to indeed try this, I wonder if they would use titanium fins or if they could rig it with aluminum fins? Very clearly would be a drone-ship landing, and the mission profile would be interesting.

Think after abort occurs (And the rocket survives) S1 would continue to MECO separate the dummy 2nd stage, and head down to land.

If it lands, this booster would go down in history.
"The Starship has landed"

Offline ZChris13

Falcon 9 stage 1 engines will be shut down as part of the abort test, commanded by the capsule. It will not be continuing on to a normalish MECO and stage seperation, even if it survives, 0119.
420 posts, nice
« Last Edit: 02/28/2019 09:14 pm by ZChris13 »

Offline Lars-J

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At the NASA social briefing just now for DM-1, Benji Reed from SpaceX (Director of Crew Management) was asked about the in-flight abort test. He said that SpaceX would ideally like to bring the booster home. So maybe they'll equip it for a return (although as Elon recent said it may well not survive).

If they hope to recover it, it’s not a MAYBE that they will include recovery hardware. It is a CERTAINTY.

(Assuming that intention does not change)

Offline Raul

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At the NASA social briefing just now for DM-1, Benji Reed from SpaceX (Director of Crew Management) was asked about the in-flight abort test. He said that SpaceX would ideally like to bring the booster home. So maybe they'll equip it for a return (although as Elon recent said it may well not survive).

If they hope to recover it, it’s not a MAYBE that they will include recovery hardware. It is a CERTAINTY.

(Assuming that intention does not change)
And in that case, they should also have ASDS on standby in the area.


Related video...
Benjamin Reed: "... so we'd like to try to bring that rocket back home..."
https://twitter.com/spacecoast_stve/status/1101307942178115588

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