Future of Orion??
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Danny Deger - 07 Mar 2007 00:51 GMT What is your opinion of the future of Orion -- especially in light of the recent budget downfalls?
My opinion is Orion will fly only because the Russians and the Chinese both have a manned program. If it wasn't for this, we would stop ours.
But then I might be wrong. I thought the need of the Navy for a new carrier based "bomber" -- especially a stealth one -- was so great they would never cancel the A-12 in the early 90's. I was wrong. The program was so messed up, they did cancel it. This might just happen to Orion.
Danny Deger
Greg D. Moore (Strider) - 07 Mar 2007 03:19 GMT > What is your opinion of the future of Orion -- especially in light of the > recent budget downfalls? [quoted text clipped - 8 lines] > > Danny Deger I thikn Orion/CEV/CLV etc is a bad mistake. But unfortunately probably can't be undone. We're rapidly approaching (and probably in some cases have passed) the point where we could continue shutle flights much beyond 2010. (Maybe we can get a couple extra tanks, but I think even that capability is fast fading. And that's really a long pole in the tent).
I think there's enough push for "We want a US presence in space" that we'll fly Orion, even if it costs more than the shuttle and does less.
I'd prefer we continued the shuttle program and used post 2010 flights to do some sort of lunar programs (there are plans out there) while looking to move to a pure commercial solution for most taxi flights.
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ed kyle - 07 Mar 2007 04:12 GMT > What is your opinion of the future of Orion -- especially in light of the > recent budget downfalls? I think that like shuttle it will be delayed by a year, or two, or three. It will come in over budget too. That is a given. There will probably be a hint of scandal at some point in the program, accompanied by a Congressional hearing and a reshuffling of program managers.
But it will fly. When it does, I think that it has a very good chance of proving to be the safest human launch system ever fielded.
- Ed Kyle
Jorge R. Frank - 07 Mar 2007 04:24 GMT > But it will fly. When it does, I think that it has a very good > chance > of proving to be the safest human launch system ever fielded. I think Orion's chances of flying over fifty flights in its entire operational lifetime are low, but assuming it does, its chances of getting through its first 58 flights without a fatal accident (which is what it will need just to match the shuttle's safety record, currently the best of any manned spacecraft) are even lower.
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ed kyle - 07 Mar 2007 05:09 GMT > > But it will fly. When it does, I think that it has a very good > > chance [quoted text clipped - 5 lines] > will need just to match the shuttle's safety record, currently the best of > any manned spacecraft) are even lower. What makes you think that?
- Ed Kyle
Jorge R. Frank - 07 Mar 2007 14:42 GMT >> > But it will fly. When it does, I think that it has a very good >> > chance [quoted text clipped - 7 lines] > > What makes you think that? Several reasons. I've been thinking about it overnight to try to rank them and right now this is the best I have:
1) Human error is the cause of 80% of aviation accidents and this pattern is continuing in spaceflight. Out of five fatal accidents (Apollo 1, Soyuz 1 and 11, STS-51L and 107), human error was a primary cause of all but Soyuz 11. Compared to this cause, all other causes are secondary (and therefore, all the safety features designed into spacecraft are likewise secondary). It's just that in spaceflight, much more of the responsibility falls on those on the ground rather than the flight crew: in the four spacecraft accidents caused by human error, the error was the decision to proceed with a launch or ground test despite indications of an unsafe condition. There is no reason to believe that Orion will be immune to this.
2) All spacecraft have design flaws; unlike aviation, we have not gone through enough design generations to weed them out. The staleness of the current US experience base due to the long gap between design generations increases the likelihood of a flaw in Orion. And Orion already has one obvious flaw, common to all current and historical capsules: the necessity of jettisoning critical parts of the spacecraft during the window between deorbit and entry interface. This design flaw was a contributing cause to the Soyuz 11 mishap and the primary cause of two close calls (Soyuz 5 and TM-5). It just doesn't get widely recognized as a flaw per se because it hasn't killed an American (yet).
3) Orion's projected flight rate is so low that I believe reusability will prove to be non-viable. That means a big hit to component reliability since Orion's systems will never get out of the "infant mortality" part of the "bathtub curve."
There are other reasons but after ranking them, I think the above three capture the "first-order" effects and a good bit of the second-order.
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Derek Lyons - 07 Mar 2007 16:04 GMT >2) All spacecraft have design flaws; unlike aviation, we have not gone >through enough design generations to weed them out. The staleness of the >current US experience base due to the long gap between design generations >increases the likelihood of a flaw in Orion. It's not like we had a significant experience base to go stale in the first place Jorge. Not only did the Mercury-Gemini-Apollo series overlap each other to a large degree, they were all essentially first generation systems.[1] Each program experienced significant flight anomalies, and in Apollo's case, had at least two inflight failures (15 docking, 17 SPS) that could easily have lead to LOM or LOCV.
The brutal fact is that we only avoided losing more crews by sheer good luck and the extremely limited number of flights. The 'experience base' and 'design generations' are non issues - because niether existed then or now.
[1] In the sense that experience with one had only an extremely limited 'feed forward' to the next.
D.
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André, PE1PQX - 07 Mar 2007 21:38 GMT Derek Lyons was zeer hard aan het denken :
>> 2) All spacecraft have design flaws; unlike aviation, we have not gone >> through enough design generations to weed them out. The staleness of the [quoted text clipped - 7 lines] > anomalies, and in Apollo's case, had at least two inflight failures > (15 docking, 17 SPS) that could easily have lead to LOM or LOCV. 2 inflight failures: What about Apollo 13 (exploded O2 tank)??
> The brutal fact is that we only avoided losing more crews by sheer > good luck and the extremely limited number of flights. The [quoted text clipped - 5 lines] > > D. A.
Derek Lyons - 08 Mar 2007 00:08 GMT >Derek Lyons was zeer hard aan het denken : >> [quoted text clipped - 11 lines] > > inflight failures: What about Apollo 13 (exploded O2 tank)?? I discounted Apollo 13 because the accident was caused by component damage during handling - unlike 15 and 17 where the causes are unknown and could easily be failure modes which are rare but inherent to the design. Apollo 13 type accidents from human error can happen even in a mature program, 15 and 17 type incidents we cannot classify as the causes are unknown.
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André, PE1PQX - 08 Mar 2007 00:31 GMT Op 8-3-2007, heeft Derek Lyons verondersteld :
>> Derek Lyons was zeer hard aan het denken : >>> [quoted text clipped - 15 lines] > > D. Then I'd like to know what happened on Apollo 15 and 17, did not know there were some accidents during those flights.
André
Derek Lyons - 08 Mar 2007 06:20 GMT >Op 8-3-2007, heeft Derek Lyons verondersteld : >> [quoted text clipped - 20 lines] >Then I'd like to know what happened on Apollo 15 and 17, did not know >there were some accidents during those flights. 15 was unable to dock to the LM during initial T&D - until 'brute forced'. 17 suffered a failure of the primary control cables across the gimbals between the SM and the SPS.
D.
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Greg D. Moore (Strider) - 08 Mar 2007 06:34 GMT > 15 was unable to dock to the LM during initial T&D - until 'brute > forced'. Which as I recall was a potential reason for aborting the mission. Since a failur to dock in lunar orbit could have been a major problem.
(and wasn't the probe reused on a Skylab mission with similar results?)
> 17 suffered a failure of the primary control cables across > the gimbals between the SM and the SPS. Hmm, wasn't aware of that one.
> D.
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Jorge R. Frank - 08 Mar 2007 13:49 GMT fairwater@gmail.com (Derek Lyons) wrote in news:45faaae3.856300171 @news.supernews.com:
>>Op 8-3-2007, heeft Derek Lyons verondersteld : >>> [quoted text clipped - 24 lines] > forced'. 17 suffered a failure of the primary control cables across > the gimbals between the SM and the SPS. You sure you got the mission numbers right? I recall the docking failure on 14, and the SPS gimbal problem on 16.
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Jorge R. Frank - 08 Mar 2007 00:20 GMT >>2) All spacecraft have design flaws; unlike aviation, we have not gone >>through enough design generations to weed them out. The staleness of [quoted text clipped - 3 lines] > It's not like we had a significant experience base to go stale in the > first place Jorge. Yes, I know that. That's what I meant by "we have not gone through enough design generations."
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ed kyle - 07 Mar 2007 16:12 GMT > >> > But it will fly. When it does, I think that it has a very good > >> > chance [quoted text clipped - 26 lines] > reliability since Orion's systems will never get out of the "infant > mortality" part of the "bathtub curve." I attribute at least some of the failures you mentioned (the U.S. failures especially) to design flaws.
It is true that Orion won't be immune to any type of failure, but I believe that it has a good chance of being measurably safer than Shuttle and Soyuz and Shenzhou, for the following reasons.
Orion should be quite a bit safer for crews than shuttle simply because it will have the launch escape system that shuttle lacks. It will be at least as safe as shuttle in the reentry phase, and probably safer because it will have a smaller, more rugged heat shield less exposed to damage and will spend less time exposed to the reentry heating phase. Yes, Orion will have to jettison its service module, but shuttle has to retract antennas, close its payload bay doors, start its APUs, etc. before reentry. Yes Orion will have to deploy parachutes, but shuttle has to fly to a precision landing, deploy landing gear, etc.
Orion has a chance to prove safer than Soyuz and Shenzhou for the following reasons. It will ride what should be a more reliable launch vehicle than either Soyuz or Shenzhou. Ares I will have one big solid motor and one liquid upper stage engine with two separation events. Both the Soyuz and the CZ-2F launchers have six propulsion units with six engines and six separation events. In reentry, Orion will have fewer modules to jettison than either Soyuz or Shenzhou.
This is all on paper, of course. Orion should, and could, prove safer, but the development has a long way to go. The CEV design was born with safety as the primary design driver in the immediate wake of the Columbia disaster. It remains to be seen if safety will remain paramount during the execution of the spacecraft's development phase.
- Ed Kyle
ed kyle - 07 Mar 2007 16:34 GMT > Ares I will have one big solid > motor and one liquid upper stage engine with two [quoted text clipped - 3 lines] > > - Ed Kyle Addendum: CZ-2F actually has a total of nine main engines on six propulsion units. Soyuz has six main engines on six propulsion units, but each engine has four primary thrust chambers - making a total of 24 main thrust chambers. There are 16 or so smaller steering thrusters as well.
- Ed Kyle
Brian Thorn - 07 Mar 2007 18:38 GMT >Yes, Orion will have to >jettison its service module, but shuttle has to retract >antennas, close its payload bay doors, start its APUs, >etc. before reentry. Before re-entry but not before the entry burn. Soyuz is committed after the burn and *must* seperate cleanly. Shuttle can make sure everything is good before committing to the burn.
Brian
Danny Deger - 07 Mar 2007 20:41 GMT >>Yes, Orion will have to >>jettison its service module, but shuttle has to retract [quoted text clipped - 6 lines] > > Brian Soyuz 5 had a failure to separate and the crew lived. The mount between the entry and orbit module failed due to heat and the entry capsule brought the crew back alive. I tried to get a failure to separate requirement into the system, but I was shot down. If you make the attachments out of aluminum and expose them to the airstream, they should fail in time for the entry capsule to flip around in time. There were also more than one separation failures in Vostok with no fatalities.
Danny Deger
Brian Thorn - 07 Mar 2007 22:39 GMT >> Before re-entry but not before the entry burn. Soyuz is committed >> after the burn and *must* seperate cleanly. Shuttle can make sure >> everything is good before committing to the burn.
>Soyuz 5 had a failure to separate and the crew lived. STS-51C Discovery had o-ring blow-by and the crew lived...
>The mount between the >entry and orbit module failed due to heat and the entry capsule brought the >crew back alive. I tried to get a failure to separate requirement into the >system, but I was shot down. If you make the attachments out of aluminum >and expose them to the airstream, they should fail in time for the entry >capsule to flip around in time. You're putting a whole honkin' load of faith in that "should" caveat... Will it always burn through, or have the Russians just been lucky (like 51C) so far?
Brian
Jorge R. Frank - 08 Mar 2007 00:37 GMT >>> Before re-entry but not before the entry burn. Soyuz is committed >>> after the burn and *must* seperate cleanly. Shuttle can make sure [quoted text clipped - 3 lines] > > STS-51C Discovery had o-ring blow-by and the crew lived... And seven other shuttle missions had foam shedding from the ET bipod ramp and the crew lived...
Just because you dodge a bullet doesn't mean you're bulletproof.
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Danny Deger - 07 Mar 2007 20:36 GMT snip
> Orion should be quite a bit safer for crews than shuttle > simply because it will have the launch escape system [quoted text clipped - 8 lines] > parachutes, but shuttle has to fly to a precision > landing, deploy landing gear, etc. And don't forget that a capsule has a good chance of bringing a crew home alive its entry flight control system fails. This was THE requirement that took NASA from winged vehicles back to capsules during the Orbital Space Plane program. The entry without flight control requirement has been watered down now, but a capsule will give the crew a good shot of surviving a passive entry.
Danny Deger
Greg D. Moore (Strider) - 07 Mar 2007 21:12 GMT > snip > [quoted text clipped - 17 lines] > been watered down now, but a capsule will give the crew a good shot of > surviving a passive entry. Right up until the parachute fails to open.
Or the de-orbit burn fails.
ultimately there are no truly passive systems. Just different re-entry failures.
> Danny Deger
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Herb Schaltegger - 07 Mar 2007 21:24 GMT On Wed, 7 Mar 2007 15:12:11 -0600, Greg D. Moore \(Strider\) wrote (in article <LUFHh.7498$PL.4233@newsread4.news.pas.earthlink.net>):
>> And don't forget that a capsule has a good chance of bringing a crew home >> alive its entry flight control system fails. This was THE requirement [quoted text clipped - 6 lines] > > Or the de-orbit burn fails. Or the landing rockets fail to fire.
Or the pressure equalization valve fails somewhere above the stratosphere with an unsuited crew.
Or toxic chemicals seep into the ECLSS suit loops.
Or the hatch "just blows" when the capsule is bobbing in the ocean . . . ;-
> ultimately there are no truly passive systems. Just different re-entry > failures. Forget the word "re-entry" and I'd agree with you. There are MANY failure modes in any complex system. Why worry about just the one phase?
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Danny Deger - 07 Mar 2007 23:56 GMT snip
> Forget the word "re-entry" and I'd agree with you. There are MANY failure > modes in any complex system. Why worry about just the one phase? You don't. You do your best to build a system to survive failures during all phases. Ascent and entry are on the top or the list because: 1. Much of the total risk is in these phases 2. An effective abort capability can be built into these phases. An escape tower during ascent and a passively stable capsule on entry.
Danny Deger
Greg D. Moore (Strider) - 08 Mar 2007 02:45 GMT > On Wed, 7 Mar 2007 15:12:11 -0600, Greg D. Moore \(Strider\) wrote > (in article <LUFHh.7498$PL.4233@newsread4.news.pas.earthlink.net>): > > Forget the word "re-entry" and I'd agree with you. There are MANY failure > modes in any complex system. Why worry about just the one phase? Agreed.
Only reason I was focussing on re-entry was because the original poster apparently was arguing capsules are inherently safer than something like the shuttle.
Reminds me of the guy who taught me the advanced cave-rescue rigging. Early levels we design our rigging by planning for failure. (i.e. backups, safeties, etc.) His level's focus was on "planning for success". Yeah, you still have belays, backups, etc, but it does change your thinking a bit.
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Jorge R. Frank - 08 Mar 2007 00:35 GMT >> >> > But it will fly. When it does, I think that it has a very good >> >> > chance [quoted text clipped - 30 lines] > I attribute at least some of the failures you mentioned > (the U.S. failures especially) to design flaws. I don't. The design flaws were there, sure, and I consider them a primary cause *if* they weren't known before flight. But in all three US accidents, the flaws *were* known before flight (or ground test) and conscious decisions were made to proceed nonetheless. In my opinion, that makes the human error the primary cause and the design flaw a contributing cause.
> It is true that Orion won't be immune to any type of > failure, but I believe that it has a good chance of > being measurably safer than Shuttle and Soyuz and > Shenzhou, for the following reasons. <snipped reasons for brevity>
> This is all on paper, of course. Good thing you included that disclaimer. The reasons you cite are all reasons why Orion *should* *theoretically* be safer. The only way Orion can *prove* itself safer is via flight record. I don't believe Orion will ever fly enough to prove that; at NASA's projected flight rates, it won't hit 58 flights until around 2040 or so.
> Orion should, and > could, prove safer, but the development has a long [quoted text clipped - 3 lines] > safety will remain paramount during the execution > of the spacecraft's development phase. Good thing you included that disclaimer too. Now you have something to point back to after Orion has its first fatality.
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Greg D. Moore (Strider) - 08 Mar 2007 02:51 GMT > Good thing you included that disclaimer. The reasons you cite are all > reasons why Orion *should* *theoretically* be safer. The only way Orion > can *prove* itself safer is via flight record. I don't believe Orion will > ever fly enough to prove that; at NASA's projected flight rates, it won't > hit 58 flights until around 2040 or so. Of course ultimately new systems have to replace old ones. But I do agree.
And this is one reason why it bothers me we're losing the shuttle. It's slowly become a mature system, and we're tossing it away for something newer and shinier.
(Personally I'd argue we would have been "better" off treating the shuttle more like the developmental system it was and simply fly more flights for the sake of more flights. the focus on "we need a payload" so we can justify the cost just made things worse. Had we dropped say another billion a year on the shuttle program just to fly 25-50% more flights and mark them as pure "development testing" probably would have created a far safer system.)
>> Orion should, and >> could, prove safer, but the development has a long [quoted text clipped - 6 lines] > Good thing you included that disclaimer too. Now you have something to > point back to after Orion has its first fatality. I dread another Mr. Fenyman interviewing NASA folks who believe Orion has a 1 in a 100,000 (or better) risk of mission failure based on sheer hope.
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Derek Lyons - 08 Mar 2007 06:22 GMT "Greg D. Moore \(Strider\)" <mooregr_deleteth1s@greenms.com> wrote:
>I dread another Mr. Fenyman interviewing NASA folks who believe Orion has a >1 in a 100,000 (or better) risk of mission failure based on sheer hope. I dread another generation learning nothing about a spacecraft accident except from Mr. Fenyman or his equivalent.
D.
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Revision - 09 Mar 2007 05:44 GMT "Derek Lyons"
> I dread another generation learning nothing about a spacecraft > accident except from Mr. Fenyman or his equivalent. You'd be lucky to have had a seat in one of his classes. Moronic insult of a Nobel Laueate.
Derek Lyons....
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Derek Lyons - 19 Mar 2007 04:48 GMT >"Derek Lyons" > >> I dread another generation learning nothing about a spacecraft >> accident except from Mr. Fenyman or his equivalent. > >You'd be lucky to have had a seat in one of his classes. Very true - but having nothing whatsoever to do with the discussion at hand.
>Moronic insult of a Nobel Laueate. Nope, a simple statement of fact.
D.
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Jorge R. Frank - 10 Mar 2007 02:59 GMT "Greg D. Moore \(Strider\)" <mooregr_deleteth1s@greenms.com> wrote in news:KSKHh.7576$PL.5321@newsread4.news.pas.earthlink.net:
> (Personally I'd argue we would have been "better" off treating the > shuttle more like the developmental system it was and simply fly more [quoted text clipped - 3 lines] > 25-50% more flights and mark them as pure "development testing" > probably would have created a far safer system.) Sentimentally I'd agree. Realistically, although the shuttle *should* have been designed and built as a "developmental" system, it was instead designed and built to be "operational". This is evident all the way down to program terminology; true developmental systems have "cockpits" and "instrument bays", not "crew cabins" and "payload bays". Unfortunately, the shuttle turned out rather too expensive to utilize in a truly developmental fashion, and has been assigned "operational" missions, of which two remain: assembling ISS and servicing HST. This will remain a source of conflict between the program and the recommendations of both accident investigation boards, unfortunately.
> I dread another Mr. Fenyman interviewing NASA folks who believe Orion > has a 1 in a 100,000 (or better) risk of mission failure based on > sheer hope. I already shudder when I hear people quote the 1:2000 LOCV risk for Orion cited in the ESAS report as if it were fact.
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Greg D. Moore (Strider) - 12 Mar 2007 04:26 GMT > Sentimentally I'd agree. Realistically, although the shuttle *should* have > been designed and built as a "developmental" system, it was instead [quoted text clipped - 10 lines] > between the program and the recommendations of both accident investigation > boards, unfortunately. Ayup. It's so easy to look back on what we "should have done".
Heck, it amazes me just some of the instrumentation being flown on the shuttle since Columbia to collect data (like the cameras).
Some of this strikes me as stuff that should have been done from day one.
Now how many flights before Orion gets called "operational"?
>> I dread another Mr. Fenyman interviewing NASA folks who believe Orion >> has a 1 in a 100,000 (or better) risk of mission failure based on >> sheer hope. > > I already shudder when I hear people quote the 1:2000 LOCV risk for Orion > cited in the ESAS report as if it were fact. Ayup. I'd be highly surprised if a) we get anywhere near 1/10th that number of flights and if we don't either have a LOCV during that time or come REAL close.
Watching FTETTM episode Spider, I was reminded of what a huge risk Apollo 8 had been. Just imagine if the LOX tank on that flight had failed.
(oh gawd, ok.. who's responsible for this quote on Wikipedia... http://en.wikipedia.org/wiki/From_the_Earth_to_the_Moon_%28TV_series%29
"That's All There Is - The story of Lunar Module Pilot Alan Bean and his experiences on the Apollo 12 mission. The episode is a humorous depiction of the most tight-knit crew to serve on an Apollo mission. On virtually all online usenet and internet episode popularity polls, such as ones conducted by Pat Flannery shortly after the series ended, this episode is consistently ranked as the best of the series."
Umm Pat?
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Herb Schaltegger - 07 Mar 2007 16:37 GMT > 2) All spacecraft have design flaws; unlike aviation, we have not gone > through enough design generations to weed them out I would argue strongly that design flaws still exist in just about every aircraft ever built and flown. They just haven't all bitten anyone on the a.s yet.
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Jan Vorbrüggen - 07 Mar 2007 17:06 GMT > I would argue strongly that design flaws still exist in just about every > aircraft ever built and flown. They just haven't all bitten anyone on the > a.s yet. Indeed. What was that thing about the 737's elevator going hard over in certain environmental conditions, first "noticed" after several decades of use of several thousand planes?
Jan
Derek Lyons - 08 Mar 2007 00:13 GMT >> 2) All spacecraft have design flaws; unlike aviation, we have not gone >> through enough design generations to weed them out > >I would argue strongly that design flaws still exist in just about every >aircraft ever built and flown. They just haven't all bitten anyone on the >a.s yet. There comes a point (I believe) where the likelihood of a major flaw remaining decreases to near zero. (I don't think it ever actually become zero.) Some design flaws can be of such an obscure nature that their likelyhood of occurence in flight is essentially zero.
D.
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André, PE1PQX - 07 Mar 2007 10:23 GMT Jorge R. Frank formuleerde op woensdag :
>> But it will fly. When it does, I think that it has a very good >> chance [quoted text clipped - 5 lines] > will need just to match the shuttle's safety record, currently the best of > any manned spacecraft) are even lower. If you are talking about US manned-launches only, your'e probably right, but if you are talking in general: take a look at the Soyuz launch record. I mean the Soyuz is an very old design (I know it had some upgrades etc.) but by my knowledge, it had only 2 or 3 fatalities since the last part of the 1960's.
http://www.russianspaceweb.com/soyuz.html
André
Greg D. Moore (Strider) - 07 Mar 2007 11:42 GMT > Jorge R. Frank formuleerde op woensdag : >>> But it will fly. When it does, I think that it has a very good [quoted text clipped - 13 lines] > > http://www.russianspaceweb.com/soyuz.html Yes, but look at how many flights it has had since its last fatal failure.
> André
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André, PE1PQX - 07 Mar 2007 11:54 GMT Na rijp beraad schreef Greg D. Moore (Strider) :
>> Jorge R. Frank formuleerde op woensdag : >>> [quoted text clipped - 14 lines] > >> André That's my point also.... those fatalities were many years ago....
Herb Schaltegger - 07 Mar 2007 13:18 GMT > Na rijp beraad schreef Greg D. Moore (Strider) : >>> Jorge R. Frank formuleerde op woensdag : [quoted text clipped - 19 lines] > > That's my point also.... those fatalities were many years ago.... No, that's not your point. The actual point was that Soyuz's flight rate is so low compared to the shuttle's that you can't make a meaningful statistical comparison.
Soyuz has also had several very serious near-misses that easily could have resulted in fatalities except for basically dumb luck.
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Greg D. Moore (Strider) - 07 Mar 2007 15:35 GMT > Na rijp beraad schreef Greg D. Moore (Strider) : >> "André, PE1PQX" <pe1pqx_geenviagra@planet.nl> wrote in message > > That's my point also.... those fatalities were many years ago.... That's what NASA said right before Columbia.
And to make matters worse, I think you could probably argue that there was more in common between STS-1 and STS-107 in terms of hardware and flight experience than Soyuz-11 and today's Soyuz-TMA craft.
So really there's far less experience with the current Soyuz craft. (and look at the number of failures the Soyuz-TMA has had, including a grossly off-course landing.)
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Jochem Huhmann - 07 Mar 2007 15:58 GMT "Greg D. Moore \(Strider\)" <mooregr_deleteth1s@greenms.com> writes:
> So really there's far less experience with the current Soyuz craft. (and > look at the number of failures the Soyuz-TMA has had, including a grossly > off-course landing.) One thing to consider is the fact that Soyuz (the launcher) has quite an impressive number of launches. It also had quite an impressive number of launch failures, though. But the number could be large enough to look at the individual failure details and to analyse if they would've been survivable if there had been a manned craft on top of it.
Because one major difference between Soyuz and STS is the fact that a launch failure with STS almost surely means loss of the crew, while this is not neccessarily the case with Soyuz.
Jochem
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Brian Thorn - 07 Mar 2007 18:12 GMT >Because one major difference between Soyuz and STS is the fact that a >launch failure with STS almost surely means loss of the crew, while this >is not neccessarily the case with Soyuz. Not really. Loss of one engine on the Shuttle means bail-out, RTLS abort, TAL abort, Abort Once Around, or perhaps a nominal mission, depending on when it happens. Loss of one engine on Soyuz means a high-risk, high-g abort on the escape tower.
Brian
Jorge R. Frank - 07 Mar 2007 14:25 GMT =?ISO-8859-15?Q?Andr=E9,_PE1PQX?= <pe1pqx_geenviagra@planet.nl> wrote in news:mn.3aab7d73c8e3df37.58901@planet.nl:
> Jorge R. Frank formuleerde op woensdag : >> [quoted text clipped - 11 lines] > right, but if you are talking in general: take a look at the Soyuz > launch record. I did.
> I mean the Soyuz is an very old design (I know it had some upgrades > etc.) but by my knowledge, it had only 2 or 3 fatalities since the > last part of the 1960's. Years aren't relevant, flights are.
Soyuz has two fatal accidents in 95 flights (1 in 47.5) and four fatalities in 228[*] person-trips (1 in 57). Soyuz has had 85 safe landings since the last fatal accident.
The space shuttle has had two fatal accidents in 117 flights (1 in 58.5) and fourteen fatalities in 698 person-trips (1 in 49.9). It had 87 safe landings between the 51L and 107 accidents.
Within the wide statistical uncertainty imposed by the small sample sizes, those numbers are essentially identical - they're all "one in fifty", give or take. (The other statistician's rule-of-thumb comes into play as well: if a single accident for either vehicle is enough to change the rankings, it's a tie.) I worded my statement as I did partly to be needlessly provocative and partly because "tied for first" is still equivalent to "has best record."
[*] - this is the only number I'm not certain of - it may be 225 but I don't have my spreadsheet handy.
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Brian Thorn - 07 Mar 2007 18:08 GMT >Soyuz has two fatal accidents in 95 flights (1 in 47.5) and four fatalities >in 228[*] person-trips (1 in 57). Soyuz has had 85 safe landings since the >last fatal accident.
>[*] - this is the only number I'm not certain of - it may be 225 but I >don't have my spreadsheet handy. It's 228.
Brian
Geoffrey - 08 Mar 2007 21:52 GMT On Mar 7, "Greg D. Moore (Strider)" <mooregr_deleteth1s@greenms.com> wrote:
> > The reasons you cite are all > > reasons why Orion *should* *theoretically* be safer. The only way Orion [quoted text clipped - 7 lines] > slowly become a mature system, and we're tossing it away for something newer > and shinier. This is a good point, but one that you don't see much on sci.space.*, where the analysis seems to usually be that anything paper is better than anything actually flying. If reliability is the goal, the best way to get it is to evolve by fixing flaws, not to throw it out and invent something new. Roughly, there were 25 successful flights between the first shuttle launch and the first failure, and about 85 flights between this and the second failure; if this trend kept on, by the technique of fixing flaws after they are revealed, you would expect roughly 300 flights before the next failure, and reliability rising asymptotically from there. (Notably, this is the technique that the Russians use. Soyuz is reliable because it has been used a lot.)
However, politically, "fix the shuttle and make it better" was a non- starter. There was no point in even proposing it; the whole point of the "replace the shuttle" politics was to *replace* the shuttle, not upgrade it.
> (Personally I'd argue we would have been "better" off treating the shuttle > more like the developmental system it was and simply fly more flights for [quoted text clipped - 3 lines] > as pure "development testing" probably would have created a far safer > system.) ==== in a different post,
> Soyuz has two fatal accidents in 95 flights (1 in 47.5) and four fatalities > in 228[*] person-trips (1 in 57). Soyuz has had 85 safe landings since the [quoted text clipped - 6 lines] > Within the wide statistical uncertainty imposed by the small sample sizes, > those numbers are essentially identical Good analysis.
It's notable-- although nobody ever does seen to note it-- that the Shuttle is actually the most reliable launch vehicle ever designed, in that no other vehicle in history ever made twenty-five successful orbital launches before the first failure, nor, for that matter, 87 launches before a second failure.
-- Geoffrey A. Landis http://www.sff.net/people/geoffrey.landis
Brian Gaff - 07 Mar 2007 09:53 GMT Well, politics gets into the way of most stuff these days, so who knows what will happen if the Democrats get into the Whitehouse. Its very odd at the moment, a Bush is going all out to control science by making key appointments under the President's wing, but is at the same time championing the manned space flight to other planets.
I suspect this is nothing to do with science, its all to do with diversion tactics, so if you find a way to get out of foreign wars while saving face, some other imperative will be used at nasa to do stuff, as they won't need a diversion.
I happen to think that culturally, and at what is really a tiny cost per person, sending people off planet will be good for us, but its precisely because you cannot explain what benefits it brings that we need to do it. We are an inquisitive race, and sooner or later it has to happen, why not now?
Brian
 Signature Brian Gaff....Note, this account does not accept Bcc: email. graphics are great, but the blind can't hear them Email: briang1@blueyonder.co.uk ______________________________________________________________________________________________________________
> What is your opinion of the future of Orion -- especially in light of the > recent budget downfalls? [quoted text clipped - 8 lines] > > Danny Deger Danny Deger - 07 Mar 2007 12:49 GMT > What is your opinion of the future of Orion -- especially in light of the > recent budget downfalls? > > My opinion is Orion will fly only because the Russians and the Chinese > both have a manned program. If it wasn't for this, we would stop ours. I have another question. Is Orion to the moon a good "practice" mission for a trip to Mars? My thoughts are it could be if NASA designed it to be, but adding features to the moon mission that will make it a good practice for Mars cost money and time, so NASA will not do these things. For example, reuse air and water would be good practice for Mars. NASA probably want do these things for a moon mission.
I think we will spend some money on attempting a moon mission, i.e. do some design and planning -- then cancel the moon mission due to costs. But, I don't think we will do much of anything towards a Mars mission.
Danny Deger
> But then I might be wrong. I thought the need of the Navy for a new > carrier based "bomber" -- especially a stealth one -- was so great they > would never cancel the A-12 in the early 90's. I was wrong. The program > was so messed up, they did cancel it. This might just happen to Orion. > > Danny Deger Derek Lyons - 07 Mar 2007 16:06 GMT >Is Orion to the moon a good "practice" mission for a trip to Mars? No.
D.
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John Doe - 07 Mar 2007 16:36 GMT > I have another question. Is Orion to the moon a good "practice" mission for > a trip to Mars? It has nothing to do with Mars, except when politicians talk. The space station has a hell of a lot more to do with a trip to mars than some glorified telephone booth barely big enough to hold a few people for a dozen days.
A real mission to mars will have to involve first either a shuttle (current or new), or development of robotics and guidance systems to allow remote assembly of mars expedition ship components in LEO.
Where the CEV might be of use in in ferrying people to/from the space station and/or the mars expedition assembly site.
Brian Thorn - 07 Mar 2007 18:18 GMT >I have another question. Is Orion to the moon a good "practice" mission for >a trip to Mars? To a certain degree, yes. It will get mission designers back into the practice of deep space operations sooner than a straight-to-Mars project would, so we should (re-)learn many lessons before we start the much higher risk Mars expeditions.
More importantly, though, Orion gets our foot in the door. "Back to the Moon" is less scary to politicians than "Go to Mars" would be both in costs and in risk. When (if) NASA proves it can handle deep space again with Orion lunar missions, it will be that much easier to get Congressional approval for the follow-on Mars program. (Unfortunately, by going down the Ares path, I don't think NASA's going to prove it can go to the moon. Those expensive rockets will leave no funding to do anything else on a reasonable time scale, and in the end Congress will say, "see, you can't even go to the moon, forget about Mars...)
Brian
John Doe - 07 Mar 2007 19:04 GMT > To a certain degree, yes. It will get mission designers back into the > practice of deep space operations sooner than a straight-to-Mars > project would, so we should (re-)learn many lessons before we start > the much higher risk Mars expeditions. Going to the moon is like a weekend camping trip. Going to Mars is a real expedition lasting more than a year.
In fact, going to Earth would be better training than going to the moon. Launching some habitat from KSC and landing it at some designated spot on earth (rough terrain etc) would be far better training since it would involve atmospheric re-entry and landing with parachutes etc. If you can do that, then you can do Mars.
Going on on a couple of camping trips to the moon is just some token compensation for killing the USA manned space programme. The lack of a true construction vehicle will ensure that NASA cannot build structures needed to go to Mars.
Besides, it isn't even a given that this CEV thing will go to the moon, and not even given that it will actually fly. They've already split the moon mission as a second step for CEV. And as time progresses, talk of an actual habitable moon base for permanent use will also vanish since there just won't be any funds for that.
And without a real cargo vessel, the USA will not be able to replace/upgrade the ISS, so when the later is ditched into the Pacific, CEV will have nowhere to go.
Brian Thorn - 07 Mar 2007 22:43 GMT >> To a certain degree, yes. It will get mission designers back into the >> practice of deep space operations sooner than a straight-to-Mars [quoted text clipped - 3 lines] >Going to the moon is like a weekend camping trip. Going to Mars is a real >expedition lasting more than a year. You forget, NASA isn't re-doing Apollo sorties. Their plan is to build a moonbase beginning with Landing No.1. That, most decidedly, will be useful for follow-on Mars operations. So will any sorties from the Moonbase that later astronauts make for exploration missions. That will really help pave the way for how to explore Mars.
Besides, if Mars is the real expedition and the moon is the weekend camping trip, then we are currently just doing jaunts around the block.
Brian
Derek Lyons - 08 Mar 2007 00:15 GMT >>> To a certain degree, yes. It will get mission designers back into the >>> practice of deep space operations sooner than a straight-to-Mars [quoted text clipped - 9 lines] >Moonbase that later astronauts make for exploration missions. That >will really help pave the way for how to explore Mars. Not really - as it has essentially zero in common with current plans. Short term revisits to Mars simply aren't in the cards - but they are the core of the Moon plan.
D.
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John Doe - 08 Mar 2007 01:08 GMT > You forget, NASA isn't re-doing Apollo sorties. Their plan is to build > a moonbase beginning with Landing No.1. So now that famous CEV is not only going to squeeze a few humans in a tiny capsule, but also carry a moon base right from its very first flight to the moon ?
Or is the first flight just going to have a shovel to do the ground breaking ceremony ? (humm, didn't Apollo also bring a shovel to dig a bit ?)
Jeff Findley - 08 Mar 2007 19:34 GMT >>> To a certain degree, yes. It will get mission designers back into the >>> practice of deep space operations sooner than a straight-to-Mars [quoted text clipped - 7 lines] > a moonbase beginning with Landing No.1. That, most decidedly, will be > useful for follow-on Mars operations. Not so much. Experience on the Moon does not necessarily apply to Mars missions. The difference in day/night cycles makes a difference in power and cooling systems for any lander/base. The difference in transit times makes your transport ships a lot different. For the moon, the little CEV is likely good enough to use as a lifeboat. A Mars mission lifeboat will have to be a lot bigger and likely more fault tolerant due to the much longer transit times.
Plus the gravity and atmosphere of Mars makes for much larger spacecraft in general, since you need a lot more fuel to take off and return to the Earth.
> So will any sorties from the > Moonbase that later astronauts make for exploration missions. That > will really help pave the way for how to explore Mars. The presence of an atmosphere on Mars, as thin as it is, makes things like spacesuit cooling systems much harder to build for a Mars miission. And the higher Mars gravity makes suit design even tougher. The lunar soil is likely harder to deal with because lack of erosion means the grains of dust are extremely sharp. Hopefully Martain dust isn't as abrasive.
> Besides, if Mars is the real expedition and the moon is the weekend > camping trip, then we are currently just doing jaunts around the > block. Sort of. LEO makes a lot of things easier due to the lack of gravity, but in some ways it's a hindrance.
Jeff
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John Doe - 08 Mar 2007 19:50 GMT > Sort of. LEO makes a lot of things easier due to the lack of gravity, but > in some ways it's a hindrance. Unless NASA buys the Starfleet warp drive designs from Paramount Pictures, it will still take a large number of months to get to and from Mars. And much of that time will be spent in 0g. Experience on the ISS and Mir has shown that many of the ECLSS systems are very hard to get right and remain reliable over a long period of time when operated in 0g.
Therefore, the space station is far more relevant to a trip to mars than some PR stunt in a weekend trip to the moon.
And the landing, takeoff, as well as habitat on mars would be very different than on the moon, especially if there is the expectation that such an expedition will draw from Martian atmosphere/ground for water, O2 and fuel for the return trip (at least to get back to mars orbit to redock with the expedition ship.
Jeff Findley - 08 Mar 2007 20:20 GMT >> Sort of. LEO makes a lot of things easier due to the lack of gravity, >> but in some ways it's a hindrance. [quoted text clipped - 4 lines] > shown that many of the ECLSS systems are very hard to get right and remain > reliable over a long period of time when operated in 0g. Mostly this has to do with the low reliability of the Elektron O2 generation system. At this point, it's unclear if US O2 generator will be more reliable. The low tech way out is just to launch with enough O2 for the entire mission instead of trying to make it from waste water.
From a NASA web page, "A man needs 0.63 kg of oxygen per day". Say this is a three year mission, so that's only about 700 kg of oxygen per person for the entire mission. Throw on a factor of safety and you can round that up to maybe 1000 kg of oxygen per person. You'll have to add some mass to that for tanks and possibly radiators (assuming its stored as LOX), but still, it doesn't seem to be orders of magnitude heavier than a few Elektrons (for redundancy) and a boat load of spare parts to keep them going.
Jeff
 Signature "They that can give up essential liberty to obtain a little temporary safety deserve neither liberty nor safety" - B. Franklin, Bartlett's Familiar Quotations (1919)
Herb Schaltegger - 08 Mar 2007 21:24 GMT > Mostly this has to do with the low reliability of the Elektron O2 generation > system. At this point, it's unclear if US O2 generator will be more > reliable. The low tech way out is just to launch with enough O2 for the > entire mission instead of trying to make it from waste water. It should be more reliable but probably won't be. Prototypes were running weeks and months-long closed-loop in the POST test chamber at MSFC back in the early 90's, but that was in a 1-g field of course.
One of the benefits to a fully closed-loop ECLSS is making your O2 not just out of waste water (which would have to be purified), but out of metabolic H20, of which the human body produces a LOT. A truly reliable O2 generator would be a boon for missions that are more than just there-and-back excursions. After all, an outpost on Deimos or an asteroid, or even a relatively nearby lunar base shouldn't require routine resupply of an element which would otherwise have to be dumped overboard due to over-abundance (as waste water).
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