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Soyuz Ballistic Re-entry 300 Miles Off Course
call-me-kenneth writes "Soyuz TMA-11, carrying a crew of three returning from the ISS, unexpectedly followed a high-G ballistic re-entry trajectory and ended up landing 300 miles off-course. The crew, including Commander Peggy Whitson and cosmonaut Yuri Malenchenko, are reportedly in good health. Soyuz capsules have previously saved the lives of the crew even after severe malfunctions that might have led to the loss of a less robust vehicle."
A capusle can "sort of fly" during reentry. You can use thrusters to change the attitude of the craft which changes the direction. This requires guidance. You usally use this because it's less stressful on the crew and you have pretty good accuracy. The ballistic trajectory is just like you said. Uncontrolled so you fall like a rock. So you spend less time slowing down in the upper atmosphere. You get to the thicker atmosphere sooner and when you do you are going faster which causes very high G deceleration. Not fun but the craft is designed to do it.
I love Jesus, except for his foreign policy.
Addendum:
According to this link: http://www.astronautix.com/flights/mireo23.htm the landing rockets failed anyway, which resulted in a hard, but survivable landing.
And according to this: http://www.jamesoberg.com/soyuz.html the crew has no control over the parachute deployment. (This is written in entry 6 B under "Special Questions)
Taken from a web forum, but I've seen similar stuff before:
http://www.airliners.net/aviation-forums/military/read.main/54404/
Soyuz (1967-Present)
Flights: 95
Failures: 4 (2 non-fatal)
Failure Rate: 4.21%
Cosmonauts Flown: 228
Fatalities: 4
Fatality Rate: 1.75%
Shuttle (1981-Present)
Flights: 116
Failures: 3 (1 non-fatal)
Failure Rate: 2.59%
Astronauts Flown: 692
Fatalities: 14
Fatality Rate: 2.02%
This is a statistical dead heat. There is simply not a big enough sample size to distinguish between a 1.75% and a 2.02% fatality rate. And the "who had an accident more recently" does not establish it either.
Both are good systems, each has respective advantages (simplicity and low-cost vs. a lot of on-orbit assembly and payload capability). It's good the world has both, and we may never know which would be safer with infinite flights.