Author Topic: ATK push for US space flight independence via Liberty  (Read 281926 times)

Online Galactic Penguin SST

Re: ATK push for US space flight independence via Liberty
« Reply #240 on: 07/09/2012 07:25 am »
I have a feeling ATK primarily choose the composite structure because they had already been paid to do it, and so could put it in their powerpoint with pictures of real hardware. Going with aluminum would mean they'd actually have to expend some of their own money to get pictures of real hardware. Make of that what you wish, either wise use of previous resources, or an example of the sunk-cost fallacy and a LEGO spacecraft/LV stack with loads of PR. I don't really care, much of it is in the eye of the beholder.


That's kind of a ridiculous statement. 

You claim that ATK dictated to LM, who is the OEM for Orion and its derivatives, that they will go with a composite structure because ATK was but a handfull of contractors working with the NESC on a pathfinder project several years ago?

And because of that they sacraficed any engineering judgment or trades and the long term technical and cost consequences associated with that just so they could stick something in a powerpoint presentation?

And that going with aluminum, which is a design LM clearly has advanced in the last several years and is definitely further along than a composite version, would cause ATK to have to spend their own capital funds?

In my opinion, these are the kind of statements that likely keep Liberty personnel from coming on this forum and unfortunately may have something to do with the comments Chris has made in the past about ATK not wanting to advertise here.  I know that would have an impact on me if I was closely associated with or worked for them.  It's just too damn hostile and short sighted.   
Hey, when everything in the whole powerpoint presentation comes from various other projects, you have to question if the design choices are based primarily on what's most efficient on first principles /or/ if it's based significantly on what's most convenient in selling the project by showing (at least at the surface level, if not on other levels... a question that is up for debate) that they're "just one step away" from implementing it.

It's not ridiculous. Look at it:

First stage: Ares I heritage.
Second Stage: Ariane V heritage.
Capsule: Orion-side-project heritage.
Launch abort: MLAS heritage.

Are all these really the best options from first principles, or were they chosen significantly because it is something that ATK has built and has a picture of and so can argue it's very close to fielding? This is clearly NOT a clearly conceived from the start, clean-sheet vehicle (that doesn't mean it's not a good one). But ATK apparently is taking to heart the concept that one "goes to war with the army you have, not the army one would like to have."

All of these things are things (other than the upper stage) that NASA started building and then rejected, either because the program got canceled or because the "alternative" way was shown to not have a significant advantage (in the judgement of those at NASA who make such decisions) over the conventional method. Obviously, ATK believes in their own PR, and I don't think they're being dishonest (except about the blackzone myth), but quite obviously NASA doesn't think MLAS is way better or that composite is way better for a capsule.

Well, such criticism is not unwanted of. Let's see what the Atlas V is made of:

First stage: Titan IV core stage heritage.
First stage engine: Zenit / Energia heritage.
Second Stage: Atlas III heritage.
Second stage engine: Atlas II/III heritage.
Control system: Atlas heritage.
Fairing: Atlas/Ariane 5 heritage.

Yet somehow this was seen as a bad, bad thing....

I know that most members (including me) were disgusted about the rocket-that-must-be-named-as-the-stick, but one should not automatically assume that the issues on it would be passed on to Liberty. My current issue with Liberty is its market case, but since ATK is all for it.....
Astronomy & spaceflight geek penguin. In a relationship w/ Space Shuttle Discovery.

Offline peter-b

  • Dr. Peter Brett
  • Full Member
  • ****
  • Posts: 649
  • Oxford, UK
  • Liked: 18
  • Likes Given: 74
Re: ATK push for US space flight independence via Liberty
« Reply #241 on: 07/09/2012 07:39 am »
First stage: Ares I heritage.
Second Stage: Ariane V heritage.
Capsule: Orion-side-project heritage.
Launch abort: MLAS heritage.
...

All of these things are things (other than the upper stage) that NASA started building and then rejected, either because the program got canceled or because the "alternative" way was shown to not have a significant advantage (in the judgement of those at NASA who make such decisions) over the conventional method.

Well, such criticism is not unwanted of. Let's see what the Atlas V is made of:

First stage: Titan IV core stage heritage.
First stage engine: Zenit / Energia heritage.
Second Stage: Atlas III heritage.
Second stage engine: Atlas II/III heritage.
Control system: Atlas heritage.
Fairing: Atlas/Ariane 5 heritage.

Yet somehow this was seen as a bad, bad thing....

The Atlas V heritage is not composed of things that NASA started building and then rejected, so I don't think your comparison is that valid.
Research Scientist (Sensors), Sharp Laboratories of Europe, UK

Offline Chris Bergin

Re: ATK push for US space flight independence via Liberty
« Reply #242 on: 07/09/2012 08:17 am »
Problem is there's also a few "Elon didn't invent it, so it sucks" or "It looks like Ares 1, uh oh!" posts too. That's my problem and also problem that whenever I try to keep the noise down, someone's always going to come out with the "oh, so you don't want negative posts then", which fraks me off.

My memory doesn't go back that far, so can your remind me: did you make comments like this back in the DIRECT days when every second comment was about how much Ares-1 is a window maker and anyone who advocates for it is Dr Death?

Cause it seems a lot of opinions were formed back then that will never be shaken. (not even with the full acoustic load of an SRB).


Heh, nice pun with the "shaken".

Yeah, that's clearly a problem for some people still - and a question (the negativity of Ares 1 for Liberty) for ATK when I speak to them.

Will be interesting to see if they come out with a big time smackdown data-a-thon quote, or a youtube video of a cute little girl saying "But I want to be an astronaut, I want to fly on Liberty".

Notably, on the acoustics, we know already is the counter for TO concerns and I'd expect our crowd to at least know that, such as:

http://www.nasaspaceflight.com/2008/12/ares-i-thrust-oscillation-meetings-encouraging-allowance-for-changes/

With a lot of data via Shuttle:
http://www.nasaspaceflight.com/2008/11/sts-126-srb-modification-thrust-oscillation-data/

The ground firings have shown its far less than expected. Then one takes into account there's a natural decouple via the "upside down" EPC set up, compared to the Ares 1 Upper Stage (per Mr Rominger at the announcement).

Everything sunshine and roses now? Nope. People will still expect it to snap in half during MaxQ, but it's assumption based. People (not space industry) were even saying (insisting) that would happen with Ares I-X and the four seg.

As far as "stop the bloody chestpumping" comments from me. I've done that on a number of threads, on a number of vehicles, including DIRECT and Ares 1, and Shuttle. It's sometimes futile, as the only way to stop the "I'm the king of the internet" types is to kick them off site, which is a last resort. So I'll keep banging on about how people need to have civil conversations about any vehicle.

Ironically, it's rare. This place is coming up on a million posts and it never has got close to the hell of sci.space, or the dark, dark days of SDC after Columbia. But if I get a sniff of that happening past moderation efforts, an issue that can actually damages this site (as it can only take a couple of members posting a lot of uncivil armwaving to give the entire site a bad reputation), then I have to protect the site.

Having me - and you all know me - post "For pity's sake, up your game" is a lot better than having a bunch of nameless moderators all using the "NSF MODERATOR" login (was an option), running around booting people off the second they say anything outside of "thanks for your comment, but if I may, I would respectfully counter with".

I'm rambling and I've got to get to work, but everyone remember this is a community, and it's a real person you're responding too. Respond to each other with that in mind.
Support NSF via L2 -- Help improve NSF -- Site Rules/Feedback/Updates
**Not a L2 member? Whitelist this forum in your adblocker to support the site and ensure full functionality.**

Offline Zachstar

  • Expert
  • Senior Member
  • *****
  • Posts: 2490
  • Washington State
  • Liked: 18
  • Likes Given: 2
Re: ATK push for US space flight independence via Liberty
« Reply #243 on: 07/09/2012 08:39 am »
Ares-1-X was not representative of Ares 1 or Liberty in the least.

Offline Paul Howard

  • Veteran
  • Full Member
  • ****
  • Posts: 466
  • Perth, Western Australia
  • Liked: 15
  • Likes Given: 25
Re: ATK push for US space flight independence via Liberty
« Reply #244 on: 07/09/2012 09:17 am »
Ares-1-X was not representative of Ares 1 or Liberty in the least.

Not that you read his post correctly, as he never said it was, but "in the least"? You mean, like the OML, the integration, the mass sim, the single SRB control, the TVC, the ascent profile.........tell me when to stop.

« Last Edit: 07/09/2012 10:17 am by Carl G »

Offline Jim

  • Night Gator
  • Senior Member
  • *****
  • Posts: 37821
  • Cape Canaveral Spaceport
  • Liked: 22052
  • Likes Given: 430
Re: ATK push for US space flight independence via Liberty
« Reply #245 on: 07/09/2012 10:38 am »

In my opinion, these are the kind of statements that likely keep Liberty personnel from coming on this forum and unfortunately may have something to do with the comments Chris has made in the past about ATK not wanting to advertise here.  I know that would have an impact on me if I was closely associated with or worked for them.  It's just too damn hostile and short sighted.   

It was false advertising (safe, simple, soon) that turned people

Offline Stephan

  • Veteran
  • Full Member
  • ****
  • Posts: 565
  • Paris
  • Liked: 1
  • Likes Given: 2
Re: ATK push for US space flight independence via Liberty
« Reply #246 on: 07/09/2012 11:08 am »

In my opinion, these are the kind of statements that likely keep Liberty personnel from coming on this forum and unfortunately may have something to do with the comments Chris has made in the past about ATK not wanting to advertise here.  I know that would have an impact on me if I was closely associated with or worked for them.  It's just too damn hostile and short sighted.   

It was false advertising (safe, simple, soon) that turned people
And the infamous EELV blackzones, still in their briefing years after it was debunked (see last ATK conference).
« Last Edit: 07/09/2012 11:09 am by Stephan »
Best regards, Stephan

Offline anonymous1138

  • Member
  • Posts: 96
  • Denver, Colorado area
  • Liked: 4
  • Likes Given: 29
Re: ATK push for US space flight independence via Liberty
« Reply #247 on: 07/09/2012 01:41 pm »
The biggest problem I have with ATK's offering is that solids cannot be shut down, and that imposes some serious design consequences on the abort system. This one is a showstopper for me, all by itself.

Offline wolfpack

  • Full Member
  • ****
  • Posts: 743
  • Wake Forest, NC
  • Liked: 160
  • Likes Given: 4
Re: ATK push for US space flight independence via Liberty
« Reply #248 on: 07/09/2012 01:55 pm »
The biggest problem I have with ATK's offering is that solids cannot be shut down, and that imposes some serious design consequences on the abort system. This one is a showstopper for me, all by itself.

They can be shut down, just not as easily as a liquid engine. STS had an early design requirement for SRB thrust termination, but it was waived for lack of a good way to do it. Basically it involves blowing another hole in the pressure chamber such that nozzle thrust becomes zero (or near zero). How you do that without rupturing the booster casing or burning up the second stage and spacecraft is the tricky part. Also tricky is the emergency detect system that would trigger such an event, as problems with solids can occur in less time than with liquids.

I'm wondering if anything of that nature is being looked at for Liberty.

Offline Downix

  • Senior Member
  • *****
  • Posts: 7082
  • Liked: 22
  • Likes Given: 1
Re: ATK push for US space flight independence via Liberty
« Reply #249 on: 07/09/2012 02:05 pm »
The biggest problem I have with ATK's offering is that solids cannot be shut down, and that imposes some serious design consequences on the abort system. This one is a showstopper for me, all by itself.

Then you'll have a problem with CST-100 too, which would fly on a solid-boosted Atlas.

ATK said that the abort system would be designed to clear any first stage failure, so the company must be using the vehicle's excess capacity to address the design challenges. 

 - Ed Kyle
The Atlas solids include thrust termination, note.
chuck - Toilet paper has no real value? Try living with 5 other adults for 6 months in a can with no toilet paper. Man oh man. Toilet paper would be worth it's weight in gold!

Offline baldusi

  • Senior Member
  • *****
  • Posts: 8371
  • Buenos Aires, Argentina
  • Liked: 2555
  • Likes Given: 8365
Re: ATK push for US space flight independence via Liberty
« Reply #250 on: 07/09/2012 02:13 pm »
I'll bring the perspective of a business man. If I was ATK, I would try to make a rocket from whatever I have experience on, I have an advanced understanding of the requirements, technological possibilities, limitations and pitfalls. In other words, the five segment might have a bad reputation for a human rated first stage (and may be rightly so, I'm not discussing either way). But can you name another company in the whole world that can pull it off better than ATK? Would you have propose that ATK starts a liquid engine development group? I don't think so.
A similar argument can be made about the rest of their decisions. If there's a single, existing, launcher that has experience with big segmented solids is Ariane 5. Their core is extremely well studied and characterized, their manufacturer understands the environment of big segmented solids. And they got lucky and had vacuum tested the air start of the engine and the core could be modified for this role.
Regarding the composite pressure vessel, I'm sure they have a lot of experience and tooling on composites, and they have probably improved a lot the process. But more importantly, even at the same mass (and that's not exactly a given), they have a profound understanding on it. It's something that ATK can do and feel comfortable doing it.
I don't think that they could use the Orion pressure vessel as is, it's over designed and heavy for a LEO vehicle. And they would have to reach some sort of arrangement with NASA, to be able to compete on the CCiCap, if I understand it correctly.
In other words, when you are competing, you usually go with what you feel comfortable doing, with what you know, and what you are great doing. I'm sure SpaceX would have loved to have ORSC RP-1 engine, and SNC would have loved to have liquid abort engine, or Blue Origin would have loved to have their New Shepard LV, and Boeing would have loved to have a human Rated RS-68k Delta IV. But you go with what you have and you know you can do on a reasonable budget. That competition, if you like high risks go play roulette.

Offline Adam K

  • Member
  • Posts: 37
  • Liked: 0
  • Likes Given: 0
Re: ATK push for US space flight independence via Liberty
« Reply #251 on: 07/09/2012 02:14 pm »
The biggest problem I have with ATK's offering is that solids cannot be shut down, and that imposes some serious design consequences on the abort system. This one is a showstopper for me, all by itself.

When would you deliberatly shut down a single motor stage during flight and would not cause mission failure?  On lift-off I can see you may want ot shut it down but, it does take liquids much longer to become flight operational than solids b/c of their complexity and nature.  That's why they need to be shut down.  Solids are much simpler in the way thrust is provided.
« Last Edit: 07/09/2012 02:15 pm by Adam K »

Offline Jason1701

  • Senior Member
  • *****
  • Posts: 2232
  • Liked: 70
  • Likes Given: 152
Re: ATK push for US space flight independence via Liberty
« Reply #252 on: 07/09/2012 02:27 pm »
The biggest problem I have with ATK's offering is that solids cannot be shut down, and that imposes some serious design consequences on the abort system. This one is a showstopper for me, all by itself.

When would you deliberatly shut down a single motor stage during flight and would not cause mission failure?  On lift-off I can see you may want ot shut it down but, it does take liquids much longer to become flight operational than solids b/c of their complexity and nature.  That's why they need to be shut down.  Solids are much simpler in the way thrust is provided.

Because if you don't shut down a failing solid it is much more likely to cause LOC. See 45th Space Wing report.

Offline Stephan

  • Veteran
  • Full Member
  • ****
  • Posts: 565
  • Paris
  • Liked: 1
  • Likes Given: 2
Re: ATK push for US space flight independence via Liberty
« Reply #253 on: 07/09/2012 02:27 pm »
And the infamous EELV blackzones, still in their briefing years after it was debunked (see last ATK conference).
Ares I was cancelled nearly two and a half years ago.  Let's leave it be.  Liberty is not Ares I.
Ed, I consider myself as an agnostic regarding Liberty, and even a bit positive (I confess, because of Astrium involvement) but I have a big problem with ATK still pushing the old "blackzones" argument.
I thought it was dead with Ares 1, but it's still alive in their speeches as we saw in the last Liberty press conference. Big disappointment, they certainly don't need that.
Best regards, Stephan

Offline Jim

  • Night Gator
  • Senior Member
  • *****
  • Posts: 37821
  • Cape Canaveral Spaceport
  • Liked: 22052
  • Likes Given: 430
Re: ATK push for US space flight independence via Liberty
« Reply #254 on: 07/09/2012 02:35 pm »
but, it does take liquids much longer to become flight operational than solids b/c of their complexity and nature. 

Not true.

Offline Adam K

  • Member
  • Posts: 37
  • Liked: 0
  • Likes Given: 0
Re: ATK push for US space flight independence via Liberty
« Reply #255 on: 07/09/2012 02:42 pm »
but, it does take liquids much longer to become flight operational than solids b/c of their complexity and nature. 

Not true.

Why are liquid started sooner than solids on every vehicle then?

Offline baldusi

  • Senior Member
  • *****
  • Posts: 8371
  • Buenos Aires, Argentina
  • Liked: 2555
  • Likes Given: 8365
Re: ATK push for US space flight independence via Liberty
« Reply #256 on: 07/09/2012 02:49 pm »
but, it does take liquids much longer to become flight operational than solids b/c of their complexity and nature. 

Not true.

Why are liquid started sooner than solids on every vehicle then?
Because once you start the solids you can't turn them off, and you can't really instrument them very well. With liquids you start them, allow for all the transients and take second to see that everything is nominal, then commit to flight (which you are once you started the solids). If something is off nominal with the liquids, you turn them off and you have an intact abort. If something is off nominal with the solids, you'd probably have a LOM/C.
« Last Edit: 07/09/2012 02:50 pm by baldusi »

Offline kirghizstan

  • Full Member
  • ****
  • Posts: 671
  • Liked: 179
  • Likes Given: 86
Re: ATK push for US space flight independence via Liberty
« Reply #257 on: 07/09/2012 02:50 pm »
but, it does take liquids much longer to become flight operational than solids b/c of their complexity and nature. 

Not true.

Why are liquid started sooner than solids on every vehicle then?

Easy answer from someone who doesn't do rocket science. 

because you can!

with a solid you ignite it and pray because you can't shut them off.  with liquids you can turn them on and make sure everything is ok because you can shut them off.

Offline kirghizstan

  • Full Member
  • ****
  • Posts: 671
  • Liked: 179
  • Likes Given: 86
Re: ATK push for US space flight independence via Liberty
« Reply #258 on: 07/09/2012 02:51 pm »
damn you baldusi i wanted to answer that question!

Offline Adam K

  • Member
  • Posts: 37
  • Liked: 0
  • Likes Given: 0
Re: ATK push for US space flight independence via Liberty
« Reply #259 on: 07/09/2012 02:54 pm »
but, it does take liquids much longer to become flight operational than solids b/c of their complexity and nature. 

Not true.

Why are liquid started sooner than solids on every vehicle then?
Because once you start the solids you can't turn them off, and you can't really instrument them very well. With liquids you start them, allow for all the transients and take second to see that everything is nominal, then commit to flight (which you are once you started the solids). If something is off nominal with the liquids, you turn them off and you have an intact abort. If something is off nominal with the solids, you'd probably have a LOM/C.

Ok, so in a sense, what you're saying is that liquids are more riskier and less reliable (based on complexity of the system) than solids based on a general need to check liquids proir to commit?  There aren't any moving parts (besides the TVC) in a solid so what would you check if you could check them?

Tags:
 

Advertisement NovaTech
Advertisement Northrop Grumman
Advertisement
Advertisement Margaritaville Beach Resort South Padre Island
Advertisement Brady Kenniston
Advertisement NextSpaceflight
Advertisement Nathan Barker Photography
0