> Star Liner has all the same problems that the Space Shuttle had. In an emergency, how do you get the crew out safely?
Starliner has a launch abort system; the Shuttle did not.
From what I understand, they use a very powerful rocket (much more powerful than Crew Dragon) to get the capsule far away from the booster. I guess it can get far enough away that NASA is satisfied that falling bits of burning SRB aren't a danger to the parachutes.
During the Starline abort test only 2 of the 3 parachutes opened, and that was a pad abort test - no SRBs!! NASA not only calling that a "success", but a sufficient success to move onto crewed testing was about the moment I lost all faith in Bridenstine being different. Immediately after leaving office he picked up a cushy consulting type gigs for various aerospace/defense companies (aka Boeing et al). Shocker.
For those who might not know SRB = solid rocket booster. Boeing uses them, SpaceX doesn't. An SRB is basically like a giant firecracker. You light it and it starts burning and doesn't stop until its done. It poses substantial safety concerns in the case of an accident where you need to abort the flight. But they're cheap, extremely powerful, and relatively simple contrasted against liquid fuel engines.
While I share your reservations with solid rockets as a main propulsion system on a manned rocket, it turns out they are well suited for launch escape systems themselves for some of the same exact reasons: they’re simple and powerful.
> While I share your reservations with solid rockets as a main propulsion system on a manned rocket, it turns out they are well suited for launch escape systems themselves for some of the same exact reasons: they’re simple and powerful.
Interestingly, both Crew Dragon and Starliner have eschewed SRB based LES/LAS systems for liquid fueled hypergolic ones. You can tell this because neither capsule has a "puller" on the nose like Apollo/Orion does.
Yeah, that is an interesting decision, especially since hypergolics represent a completely different set of risks. But they are extremely reliable for this application.
Well we shall see I suppose. SRB's go back to the Apollo era and NASA safety qualifications often come down to 'are you doing what we've done before'? Hence them refusing to even consider SpaceX retropulsive crew landings, even though that would be a huge step forward.
I would also observe that NASA has a relatively poor safety record contrasted against the Soyuz (which has not lost crew since 1971 in spite of flying more manned missions), and one of the few completely catastrophic crashes we have had, Challenger, was directly related to the SRB. In either case, I expect variance is playing a much larger role than most might appreciate.
Didn't the shuttle have this harebrained thing where the crew were supposed to climb all the way to the exit hatch in their pressure suits, extend a boom along the wing in full flight and then parachute out along it?
I thought I read about that. Of course that's effectively no actual escape system lol. They'd be long dead by the time they managed all that in an out of control shuttle.
Yep. That's supposedly for them to ditch in the event that the main engines fail but the shuttle is controllable - they don't have enough energy for a trans-atlantic abort, so they glide and bail out over the ocean.
How far did this plan go? Just because it was discussed and documented and thought through does not mean it was something that was actually going to happen. Was this actually developed and the parts&pieces put into place with procedures written up in the flight manual?
> Did the astronauts believe that it's likely that the system would save them? Probably not.
Yeah personally I would have taken my chances ditching the craft, tbh. It would probably ditch pretty well considering it doesn't have huge engine pods under the wings.
