Shenzhou  
Initial Operational Capability (IOC): 2011
Maiden Flight: 15 October 2003
Total Production: 7
Origin: China
Parent System: Shenzhou
Initial Operational Capability (IOC): 2011
Maiden Flight: 15 October 2003
Total Production: 7
Reviews
There are no reviews so far

Write your review

Description: The Shenzhou, 'Divine Ship of the Gods' in English, is a modular, expendable, spacecraft developed and operated by the People's Republic of China to support its manned space program. It was developed in the 1990s and early 2000s with the first manned test launch (Shenzhou 5) completed on October 15, 2003. Four previous unmanned test flights were carried out in 1999 (1), 2001 (1) and 2002 (2). The second manned flight (Shenzhou 6) was carried out on October 12, 2005. The third flight (Shenzhou 7) carried out on September 25, 2008, involved the first spacewalk of two members of a crew of three-man. The Shenzhou spacecraft is launched by a Long March 2F rocket from Jiuquan Satellite Launch Center. The Shenzhou 8 due to launch in 2011 is expected to become the final design of the spacecraft encompassing all the improvements which lacked in the previous spacecrafts.
The Shenzhou spacecraft is similar to the Russian Soyuz. It has three modules: orbital module in the forefront, re-entry module in the middle and service module in the aft. The main difference is that the orbital module has its own propulsion, control systems and solar panels. The orbital module is designed to accommodate the crew during their mission in orbit. The re-entry module is the only section designed to return to the Earth's surface. The service module contains the engines, solar panels and instruments.
China is preparing the Tiangong-1 space module scheduled for launch in 2011 to create its first space station along with three Shenzhou spacecrafts (8, 9 and 10). In 2012 the new space station will receive the first spacecraft replacement docking with the Shenzhou 11.

Shenzhou Applications


Space Launch Systems ChangZheng 2F

Shenzhou Specifications

Crew: 3
Dimensions
Diameter: 2.80 meter
Length: 9.25 meter (30.3 foot)
Solar Panel Span: 17 meter
Performance
Orbit: 341 kilometer (212 mile)
Time
Mission Endurance: 20 day (0.05 year)
Service Life: 20 day
Weight
Max Takeoff Weight: 7,840 kilogram (17,284 pound)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Operators & Related Equipment


OperatorsItems

Grand Total 71
 

Shenzhou Ship Listing


SerialNameStatusLaunch DateCommissionDecommission
Shenzhou V-15 Oct 200329 Oct 2003
Shenzhou VI-12 Oct 200517 Oct 2005
Shenzhou VII-25 Sep 2008Oct 2008
Shenzhou VIII-1 Nov 2011-
Shenzhou IX-2012-
Shenzhou X-11 Jun 201326 Jun 2013
Shenzhou XI-2014-

Shenzhou Links & Resources

Copyright © 2003-2014 deagel.com website. All rights reserved.
This website has been optimized for HTML 5 and CSS 3.