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Would it be reasonable to expect the Shenzhou desent profile to be similar
to Soyuz? I guess from an aerodynamic point of view there can't be much dufference since the modules are quite similar in size and shape? What is the approx timespan from de-orbit burn completion until touchdown of Souyz? BTW: Xinhua reports at 2137 GMT that SZ5 has performed the initial maneuvers prior to de-orbit burn. According to some sources touchdown is expected approx 2230 GMT. /Nikolaj |
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Thread | Thread Starter | Forum | Replies | Last Post |
SRB Thrust Profile | Charles Talleyrand | Space Shuttle | 7 | October 15th 03 01:01 PM |
Chinese TV/Radio Coverage of Shenzhou | James Oberg | Space Shuttle | 2 | October 11th 03 04:41 PM |
Dynamic re-entry profile ? | Adam Darren | Space Shuttle | 5 | September 29th 03 01:55 PM |
Question: Soyuz Descent Module Landing System | John Pelchat | Space Science Misc | 3 | August 22nd 03 08:30 AM |