Author Topic: SpaceX Falcon Heavy : Arabsat 6A : LC-39A : April 11, 2019 - DISCUSSION  (Read 308835 times)

Offline 49er

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It seems to me that the peak velocity of the boosters in space is irrelevant to the velocity of the boosters after they complete their individual re-entry burns.  Is there any evidence that the center booster is traveling any faster than the side boosters at the point when it first encounters the top of the atmosphere?  The timing of the callouts for "subsonic" and "start of landing burn" seems very similar in both instances.

Offline mme

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If the reason they are shutting down engines is to limit G-loading, wouldn't it make more sense to shut down engines on the center core than on the boosters?  This would allow them to burn more propellant on the side boosters than the center core, and would slightly improve payload.  3 of the center core engines are restartable, any engines that were shut down could be re-lit after staging.
They can only relight the engines as long as they still have TEA-TEB in the tanks. The center core on the first FH launch failed to land because it ran out of it during the landing burn startup so I guess the margins are already pretty tight.
It's also safer to not have to restart engines in flight for the success of the primary mission. I also think they are unloading the struts [1] in preparation for separation.

[1] I forgot the proper term for the connecting rods on the top of the boosters...
« Last Edit: 04/12/2019 05:23 pm by mme »
Space is not Highlander.  There can, and will, be more than one.

Offline Lars-J

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ISTM that the "toastiness" of a given stage should be able to be managed by the duration of the re-entry burn (assuming you have the propellant to burn).  If that's the case, then where do the comments about variable levels of "toastiness" come from?

Keep in mind that the boosters will always get toasted a bit by the center core during separation, that can't be avoided. But I'm not sure much much that contributes to the final "toastiness".

Offline Vettedrmr

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Keep in mind that the boosters will always get toasted a bit by the center core during separation, that can't be avoided. But I'm not sure much much that contributes to the final "toastiness".

I think of that toasting as a "light caramel glazing" ;)

Have a good one,
Mike
Aviation/space enthusiast, retired control system SW engineer, doesn't know anything!

Online crandles57

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It seems to me that the peak velocity of the boosters in space is irrelevant to the velocity of the boosters after they complete their individual re-entry burns. 

I would assume that to minimise fuel use, reentry burn is timed to be at last few seconds possible to prevent booster getting too hot, ie some toastiness applied before re-entry burn (though atmosphere is thin at this stage). Not sure if you are suggesting that the engines can only be relit in vacuum or thick atmosphere but not in thin atmosphere and therefore re-entry burn is timed to be before hitting atmosphere or if this pre-entry burn part of the toastiness is completely unimportant or something else?


Edit: I assume that on a more challenging mission/faster peak speed the reentry burn is at higher altitude and also cuts off at higher altitude and speed is still higher than on a less challenging mission. Speed builds up again from higher altitude so longer/stronger landing burn is also required on the more challenging mission. So there is also more toastiness between entry burn and landing burn as well as pre re-entry burn.
« Last Edit: 04/12/2019 06:19 pm by crandles57 »

Offline 49er

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I was discussing a question I asked  little earlier in the thread about why downrange landings are referred to as toasty while RTLS landings are not.  The answer I originally got was because the booster is moving faster at staging.

My question was that since the re-entry burn is over twice as long for a drone ship landing, isn't the atmospheric re-entry speed (which could be assumed to be toasting the booster)  about the same for both landing scenarios?  The velocity telemetry wasn't shown for the re-entering boosters, but the subsonic and landing burn callouts are very similar for the two types of landings so shouldn't the initial re-entry speeds be about the same with neither one being more toasty than the other.

In other words, is it something other than atmospheric re-entry heating that the web-cast commenters are talking about when they say the booster is toasty?  It seems to me that sootiness from the retro burn shouldn't be called toasting unless it actually heats up the booster significantly.  Does it?

Probably as  a result of my operator error, my follow-on question did not append to my original question.  My bad!

Offline Barley

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To date there have been several hundred air starts (second stage) and restarts (first stage recoveries) so there should be a high degree of confidence that an engine will start when asked.

A simple failure to restart may not result in a loss of the primary mission.  They could burn the landing fuel, expending the booster, to compensate for the lower thrust.

Shutting down and restarting an engine may be more risky than other options, but it doesn't look like it's so many orders of magnitude more risky that it could never be contemplated.

Online crandles57

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49er,
I think I have understood that the 'sootiness' is not soot, it is scorching from re-entry heat. (They don't wash off the soot because it isn't soot.) So I believe blacker look is caused by re-entry heat.


You seem to be assuming the re-entry burn is before entering atmosphere. I am assuming it is, for a challenging high speed mission, to be at last possible few seconds to prevent temperature reaching critical design limit temperature. i.e. re-entry burn occurs after re-entry has started.

Speed and thickness of atmosphere contribute to heat. So higher speed mission heats up more at higher altitude (atmosphere thinner but speed faster to get same heating effect).  So you get differences in: length/strength of re-entry burn, altitudes at which re-entry burn occurs and probably also in length/strength of landing burns.
« Last Edit: 04/12/2019 06:54 pm by crandles57 »

Offline Lars-J

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49er,
I think I have understood that the 'sootiness' is not soot, it is scorching from re-entry heat. (They don't wash off the soot because it isn't soot.) So I believe blacker look is caused by re-entry heat.

It's actually a bit of both. Note how they cleaned/polished up the first reused booster quite a bit. (BulgariaSat 1, see image) It was not repainted. So most of it just soot.

For later launches they decided that deep level of cleaning was not needed.
« Last Edit: 04/12/2019 07:23 pm by Lars-J »

Offline obi-wan

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Good to see all three booster cores down safely and to hear that the fairings are down intact and in reusable condition.

If nothing else, Elon Musk can rightfully claim to have changed the face of rocketry. What was previously considered to be so high-concept that only NASA or some other state space agency could possibly attempt it has been achieved by SpaceX instead: Mostly-reusable launch vehicles with loss of hardware pulled down to a bare minimum.

The paradigm has changed; ULA, Arianespace and all the other developers and manufactures of launch vehicles now have to accept and follow the path SpaceX and Blue Origin are treading. Any launch vehicle that does not include reusable boosters is going to have a hard time surviving the bean-counters' scrutiny.
I am amazed and appalled that SpaceX has never been awarded the Collier Trophy (basically the Nobel Prize for aerospace engineering). As I understand it, they haven’t even been a finalist since the last Falcon 1 flight. I think Falcon Heavy alone deserves it; if they fly two FH missions this year and fly crew to ISS, they better win it for 2019!

Online crandles57

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It's actually a bit of both. Note how they cleaned/polished up the first reused booster quite a bit. (BulgariaSat 1, see image) It was not repainted. So most of it just soot.

For later launches they decided that deep level of cleaning was not needed.

Hmm, perhaps that serves me right for believing Musk.

https://twitter.com/elonmusk/status/1068940024136126464?lang=en
"Reentry scorchmarks, not simple soot. Can’t wipe it off."

Are you saying Musk is lying / being misleading?

.

Iridium 8 reentry burn started at speed of circa 4540km/h and altitude of 46.8km and runs for ~16 secs until speed down to about 3060km/h at 31.7km altitude.


Do we have such stage 1 telemetry or similar from a GTO launch?


Offline whitelancer64

Good to see all three booster cores down safely and to hear that the fairings are down intact and in reusable condition.

If nothing else, Elon Musk can rightfully claim to have changed the face of rocketry. What was previously considered to be so high-concept that only NASA or some other state space agency could possibly attempt it has been achieved by SpaceX instead: Mostly-reusable launch vehicles with loss of hardware pulled down to a bare minimum.

The paradigm has changed; ULA, Arianespace and all the other developers and manufactures of launch vehicles now have to accept and follow the path SpaceX and Blue Origin are treading. Any launch vehicle that does not include reusable boosters is going to have a hard time surviving the bean-counters' scrutiny.
I am amazed and appalled that SpaceX has never been awarded the Collier Trophy (basically the Nobel Prize for aerospace engineering). As I understand it, they haven’t even been a finalist since the last Falcon 1 flight. I think Falcon Heavy alone deserves it; if they fly two FH missions this year and fly crew to ISS, they better win it for 2019!

Other aerospace achievements overshadowed SpaceX (Blue Origin won for the first booster landing). If it flies crew first, then it should get a very strong nomination for flying crew on the Dragon.
"One bit of advice: it is important to view knowledge as sort of a semantic tree -- make sure you understand the fundamental principles, ie the trunk and big branches, before you get into the leaves/details or there is nothing for them to hang on to." - Elon Musk
"There are lies, damned lies, and launch schedules." - Larry J

Offline HeartofGold2030

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Good to see all three booster cores down safely and to hear that the fairings are down intact and in reusable condition.

If nothing else, Elon Musk can rightfully claim to have changed the face of rocketry. What was previously considered to be so high-concept that only NASA or some other state space agency could possibly attempt it has been achieved by SpaceX instead: Mostly-reusable launch vehicles with loss of hardware pulled down to a bare minimum.

The paradigm has changed; ULA, Arianespace and all the other developers and manufactures of launch vehicles now have to accept and follow the path SpaceX and Blue Origin are treading. Any launch vehicle that does not include reusable boosters is going to have a hard time surviving the bean-counters' scrutiny.
I am amazed and appalled that SpaceX has never been awarded the Collier Trophy (basically the Nobel Prize for aerospace engineering). As I understand it, they haven’t even been a finalist since the last Falcon 1 flight. I think Falcon Heavy alone deserves it; if they fly two FH missions this year and fly crew to ISS, they better win it for 2019!

Other aerospace achievements overshadowed SpaceX (Blue Origin won for the first booster landing). If it flies crew first, then it should get a very strong nomination for flying crew on the Dragon.

What achievements exactly? Also that was the DC-X...

Offline Lars-J

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It's actually a bit of both. Note how they cleaned/polished up the first reused booster quite a bit. (BulgariaSat 1, see image) It was not repainted. So most of it just soot.

For later launches they decided that deep level of cleaning was not needed.

Hmm, perhaps that serves me right for believing Musk.

Are you saying Musk is lying / being misleading?

Not at all, trust Elon :). I said it was both, but certainly could be wrong about what the primary cause of the look is. (I seem to recall images of recovered boosters where some has been wiped away) And maybe my recollection of the BulgariaSat booster not being painted is wrong.

EDIT: Here you can see where rain water has caused some soot to run down the length of the core.
« Last Edit: 04/12/2019 08:31 pm by Lars-J »

Offline whitelancer64

Good to see all three booster cores down safely and to hear that the fairings are down intact and in reusable condition.

If nothing else, Elon Musk can rightfully claim to have changed the face of rocketry. What was previously considered to be so high-concept that only NASA or some other state space agency could possibly attempt it has been achieved by SpaceX instead: Mostly-reusable launch vehicles with loss of hardware pulled down to a bare minimum.

The paradigm has changed; ULA, Arianespace and all the other developers and manufactures of launch vehicles now have to accept and follow the path SpaceX and Blue Origin are treading. Any launch vehicle that does not include reusable boosters is going to have a hard time surviving the bean-counters' scrutiny.
I am amazed and appalled that SpaceX has never been awarded the Collier Trophy (basically the Nobel Prize for aerospace engineering). As I understand it, they haven’t even been a finalist since the last Falcon 1 flight. I think Falcon Heavy alone deserves it; if they fly two FH missions this year and fly crew to ISS, they better win it for 2019!

Other aerospace achievements overshadowed SpaceX (Blue Origin won for the first booster landing). If it flies crew first, then it should get a very strong nomination for flying crew on the Dragon.

What achievements exactly? Also that was the DC-X...

Blue Origin won in 2016 “for successfully demonstrating rocket booster reusability with the New Shepard human spaceflight vehicle through five successful test flights of a single booster and engine, all of which performed powered vertical landings on Earth,” per the statement from the National Aeronautic Association.

DC-XA only flew to a maximum of 10,300 ft.
"One bit of advice: it is important to view knowledge as sort of a semantic tree -- make sure you understand the fundamental principles, ie the trunk and big branches, before you get into the leaves/details or there is nothing for them to hang on to." - Elon Musk
"There are lies, damned lies, and launch schedules." - Larry J

Offline acsawdey

Blue Origin won in 2016 “for successfully demonstrating rocket booster reusability with the New Shepard human spaceflight vehicle through five successful test flights of a single booster and engine, all of which performed powered vertical landings on Earth,” per the statement from the National Aeronautic Association.

DC-XA only flew to a maximum of 10,300 ft.

New Shepherd is the Boeing 247 to Falcon 9's DC-3. Not sure what that makes the DC-X.

Online abaddon

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There's obvious soot patterns at the top of the boosters (where you'd expect it from going through the center core plume).  Let's not overthink this.

Offline whitelancer64

Blue Origin won in 2016 “for successfully demonstrating rocket booster reusability with the New Shepard human spaceflight vehicle through five successful test flights of a single booster and engine, all of which performed powered vertical landings on Earth,” per the statement from the National Aeronautic Association.

DC-XA only flew to a maximum of 10,300 ft.

New Shepherd is the Boeing 247 to Falcon 9's DC-3. Not sure what that makes the DC-X.

More akin to the Flyer 3.
"One bit of advice: it is important to view knowledge as sort of a semantic tree -- make sure you understand the fundamental principles, ie the trunk and big branches, before you get into the leaves/details or there is nothing for them to hang on to." - Elon Musk
"There are lies, damned lies, and launch schedules." - Larry J

Offline envy887

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Terrific launch for SpaceX, and at a key moment with NSSL and NASA's SLS frustration underway. 

I have only one note about the news coverage.  Repeatedly, it is written that Falcon Heavy is "the world’s most powerful operational launcher", etc., which technically is true in terms of liftoff thrust, but FH-2 only put 6,465 kg into GEO-1500-ish m/s.   That's only 64% or so of what Ariane 5 ECA has boosted to an equivalent orbit.  All of that thrust is neat, but much of it is not being used for the actual payload mission.

 - Ed Kyle

Power isn't a good metric for measuring payload capacity. But FH can easily beat A5 ECA on either.
It could, in expendable mode, but SpaceX doesn't seem to be planning to use it that way.  I'm not sure it would cost less than an Ariane 5 if flown expendably.

 - Ed Kyle

SpaceX has claimed 10,000+ kg to GTO with 3x downrange landing. A5 ECA has never lifted 10,000 kg to GTO, and 3x downrange landing would definitely be cheaper, though they might need another ASDS.

They also claimed ~24,000 kg to GTO with center core expended for $95 million. Both cheaper and more performant than A5 ECA, and a second East Coast landing ship being built suggests that they actually plan to sell this type of launch.

Also, a fully expendable launch was quoted at $150 million. Can you actually get a A5 ECA for $150 million? I thought they were closer to $165 million.

Offline envy887

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Terrific launch for SpaceX, and at a key moment with NSSL and NASA's SLS frustration underway. 

I have only one note about the news coverage.  Repeatedly, it is written that Falcon Heavy is "the world’s most powerful operational launcher", etc., which technically is true in terms of liftoff thrust, but FH-2 only put 6,465 kg into GEO-1500-ish m/s.   That's only 64% or so of what Ariane 5 ECA has boosted to an equivalent orbit.  All of that thrust is neat, but much of it is not being used for the actual payload mission.

 - Ed Kyle

If you expended all 3 cores, (and enlarged the fairing, strengthened the payload adapter) how much can the FH boost to the same orbit? if it's more than Ariane 5 ECA then 'the world's most powerful launcher' is a fair statement.

FH, about ~20,000 kg to GTO flying full expendable.

SpaceX advertises 26,700 kg fully expended. Of course, that is to GTO-1800 and not GTO-1500.

https://www.spacex.com/about/capabilities
« Last Edit: 04/12/2019 09:18 pm by envy887 »

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