Further Details From Soyuz Mishap
fyc brings us some information from Universe Today about what happened to Soyuz TMA-11 when it re-entered the atmosphere late last week. Reports indicate that a failure of explosive bolts to separate the Soyuz modules delayed the re-entry and oriented the capsule so the hatch was taking most of the heat, rather than the heat shields. CNN reports that the crew was in 'severe danger.' They experienced forces of up to 8.2 gravities. NASA officials have voiced their approval of how Russia handled the crisis. They expect to rely heavily on Soyuz spacecraft once the shuttles are retired in 2010.
It is interesting that the GAO has concerns about the ability of Soyuz to take the shuttle's place. And anything else with capabilities that approach the shuttle's are basically vaporware at this point. I think that it is not out of line to ask if the ISS is going to make it. I'm not saying that because I think it wont, I just don't think it is to difficult to imagine very realistic scenarios where it does not.
It's hard to believe that's how Micronians are made. Why don't we see it right now by having you both kiss one another?
In soviet Russia, bolts explode you!
Knowledge is power. Knowledge shared is power lost.
It will be interesting to see public outcry when one of the Russian craft craters with Americans onboard. This will inevitably happen, even if the Soyuz is safer than anything America has (which it probably is). Then we'll all have to be dragged through a lot of media-driven "soul-searching" about whether it was smart to "outsource NASA" (you heard it here first).
Sounds very similar to the Soyuz 5 rentry (http://en.wikipedia.org/wiki/Soyuz_5), would have been quite an ordeal. For more 'interesting' reentries have a look at http://en.wikipedia.org/wiki/List_of_space_disasters
GPLv2: I want my rights, I want my phone call! DRM: What use is a phone call, if you are unable to speak?
It's interesting that it reentered safely without using the heat shield. What part of the design helped that?
There's a moral that applies here... how does it go again? Something about not putting all your eggs in one basket, if I recall correctly...
A-Bomb
I'm continually amazed by how robust and dependable the Soyuz modules are.
They're the Volvos of the space program.
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~ |rip/\/\aster /\/\onkey
People have willingly endured 46.2g 's.
try { do() || do_not(); } catch (JediException err) { yoda(err); }
The "hatch first" story is already in doubt, latest info says separation of the entry module was delayed, it entered sideways and computer thus went to ballistic mode after a certain time and was in said mode when it finally separated.
I just read a forum where knowledgeable people translate from a reliable known guy on a russian forum. Not much official has yet been revealed.
Details here
Don't know where you got that figure from.
Modern fighter aircraft are software-limited to 9G maneuvers, with the crew in G-suits and trained for it. (The hardware can probably take higher). The Gemini launches on converted Titan-II missiles routinely hit about 8G during the ascent (Shuttle does 3G).
Then-Captain John Stapp in his rocket sled experiments in the late 1940s/early 1950s routinely experienced 18G in the "eyeballs in" position, and 30G in "eyeballs out" deceleration as the sled stopped. The peak force he survived was around 45G. (Black-eyed, bloodshot, bruised, with the occasional cracked rib and generally beat up, but survived.)
-- Alastair
There's an alternative to waiting 5 years after the final shuttle launch - check out http://www.directlauncher.com./ It'd be ready 2 years after the final shuttle launch and it would cost a heck of a lot less than Ares...
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Back in the old days: "We don't fully understand the physics of this thing, so let's make this part 5 times stronger than it has any reason to be, just in case shit goes seriously wrong."
*kaboom*
"Heh, good thing we had that margin of error!"
Modern engineering: "We can shave 0.37% off the cost of the final product by replacing this part with cheaper, lighter materials. The computer model tells us this is perfectly safe to do."
*KABOOM*
"Oops, I guess our computer model didn't account for turbulence."
The incident to which you refer was a mid-air collision in an Israeli Air Force training flight. Here is a link to the History Channel interview with the pilot. After McDonnell Douglas analyzed the accident, they concluded that the F-15's lifting body design allowed it to remain airborne on one wing, given enough speed.
Gigantic kudos to the pilot who brought that plane home safely! After a full investigation into the accident, a new wing was fitted, and the fighter returned to service.
How's that for American aircraft ruggedness! (Well, in the F-15's case anyway)
Cole's Axiom: The sum of the intelligence on the planet is a constant. The population is growing.
http://www.hobbyspace.com/nucleus/index.php?itemid=5989&catid=49 NASA needs the Falcon 9/Dragon combo to attain crew service capability if the agency is to have a US based option for sending astronauts to the ISS sometime during the period between the end of the Shuttle program in 2010 and the start of Ares I/Orion operations in 2015. So far, all the designs reviews (e.g. here, here, and here) have found no fundamental flaws in either the Falcon 9 or Dragon designs. Assuming aerospace engineering does not involve black magic, this should mean something. Currently COTS is funding F9/Dragon (and also the Orbital Taurus II) only for cargo services. Increasing COTS funding to accelerate development of the Dragon for crew transport would seem a reasonable gamble, especially considering it would cost a fraction of what is going into the Ares/Orion program.
On the other hand, if Falcon 9/Dragon succeeds there will most likely arise overwhelming pressure to kill Ares I/Orion to save billions dollars in further development and operational costs. (NASA could alter its lunar exploration architecture to use the Dragon instead of Orion, e.g. see this powerful option.) Jeff Foust and Rand Simberg comment on recent statements from Mike Griffin as he tries to deal with this situation:
[Update: Jon Goff also discusses the gap and COTS issues: Gap Math - Selenian Boondocks - Apr.8.08.]
Well that's stupid. Everyone knows the space station is like one of those buddhist sand painting thingies. It's about the building, not the having.
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Please remember that brave and slightly insane man survived 45G for a tiny fraction of a second. Any longer they would have problems separating him from the rest of the rocket sled.
8G during reentry is bad enough for me, thanks. It must feel like quite a beating.
http://www.dieblinkenlights.com
pilots tend to black-out or grey-out around 9 or 10 Gs when flying aircraft, spacecraft pilots can go a bit higher because of more favorable seating positions.
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