Еще о китайском космическом корабле

Теги:авиация
 
?? Serge Pod #05.12.1999 09:24
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Serge Pod

администратор

Вывоз тела

http://solar.cini.utk.edu/~mwade/graphics/p/p921lv1f.jpg [zero size or time out]

На стартовой позиции

http://solar.cini.utk.edu/~mwade/graphics/c/cz2fvup.jpg [zero size or time out]

Старт



ЦУП

http://solar.cini.utk.edu/~mwade/graphics/p/p9mc20.jpg [zero size or time out]

Оно самое

http://solar.cini.utk.edu/~mwade/graphics/p/p9inorb2.jpg [zero size or time out]

http://solar.cini.utk.edu/~mwade/graphics/p/p921911b.jpg [zero size or time out]

http://solar.cini.utk.edu/~mwade/graphics/p/p9full.jpg [zero size or time out]

http://solar.cini.utk.edu/~mwade/graphics/p/p9retro2.jpg [zero size or time out]

Спуск

http://solar.cini.utk.edu/~mwade/graphics/p/p9chuted.jpg [zero size or time out]

Кокпит
http://solar.cini.utk.edu/~mwade/graphics/p/p9cockpt.jpg [zero size or time out]

Орбитальный модуль

http://solar.cini.utk.edu/~mwade/graphics/p/p9omshop.jpg [zero size or time out]

Китайский космонавт

http://solar.cini.utk.edu/~mwade/graphics/t/taikon4.jpg [zero size or time out]


http://solar.cini.utk.edu/~mwade/graphics/p/proj921.jpg [zero size or time out]

921 Spacecraft - Earlier conjectural drawing of Project 921 first Chinese manned spacecraft, based on description of its layout and overall mass. - Credit: © Mark Wade

http://solar.cini.utk.edu/~mwade/graphics/p/p921lvd.jpg [zero size or time out]

http://solar.cini.utk.edu/~mwade/graphics/c/cz2f.jpg [zero size or time out] Chinese Launch Vehicles for Manned Projects. From left: Tsien Spaceplane Launcher, 1978; Project 921 Launch Vehicle, 1992; CZ-2F, 1999; CZ-2E(A), 2000. Only the last two were put into full scale development. - Credit: © Mark Wade

Description of the Shenzhou Spacecraft
A preliminary estimate of the dimensions and mass breakdown of the Shenzhou, in comparison with the Soyuz, would be as follows:


Soyuz Shenzhou
Complete Spacecraft:
Total Mass-kg 7,250 8,400
Length-m 7.5 7.9
Diameter-m 2.7 2.5

Service Module
Total Mass- kg 2,950 3,200
-of which, propellant,kg 900 1,100
Length-m 2.3 2.3
Diameter-m 2.3 2.2
Diameter base-m 2.7 2.5

Re-entry Vehicle
Total Mass-kg 3,000 3,000
Length-m 2.2 2.2
Diameter-m 2.2 2.2

Orbital Module
Total Mass-kg 1,300 2,200
Length-m 3.0 3.4
Diameter-m 2.3 2.8



In knowledge we trust!  

tHARM

втянувшийся
А что такие фотки размытые, интересно?
 
AD Реклама Google — средство выживания форумов :)
?? Serge Pod #08.02.2000 12:41
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Serge Pod

администратор

Pod'em na poverhnost'
Ssylki pohje sdohli.
In knowledge we trust!  

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