Shenzhou-1

Overview

Destination: Low Earth Orbit
Mission: Human Exploration

Low Earth Orbit Launch Area 4 (SLS-1 / 921) Jiuquan Satellite Launch Center, People's Republic of China

First test flight of the Shenzhou spacecraft, without crew on board. The spacecraft used has only 8 of the 13 sub-systems on board being operational, and was not equipped with a life support system or an emergency escape system. The major test objectives of the mission were the flight of the Long March 2F rocket, separation of the modules, attitude control, lifting body reentry, heat shield testing and ground recovery.

Long March 2F

Family:
Configuration: F

The Long March 2F is a Chinese orbital carrier rocket, part of the Long March 2 rocket family. Designed to launch the crewed Shenzhou spacecraft, the Long March 2F is a human-rated two-stage version of the Long March 2E rocket, which in turn was based on the Long March 2C launch vehicle. It is launched from complex SLS at the Jiuquan Satellite Launch Center.

Specifications
  • Stages
    2
  • Length
    62.0 m
  • Diameter
    3.35 m
  • Fairing Diameter
    3.35 m
  • Launch Mass
    464.0 T
  • Thrust
    5985.0 kN
Family
  • Name
    Long March 2F
  • Family
  • Variant
    F
  • Alias
  • Full Name
    Long March 2F
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    8400.0 kg
  • Geostationary Transfer Orbit
  • Direct Geostationary
  • Sun-Synchronous Capacity

Shenzhou 1


Active Human Rated Unmanned Crew Capacity: 3
Destination: Low Earth Orbit
Serial Number: 1

The first Shenzhou spacecraft was different from those later used. Instead of featuring unfolding solar panels, Shenzhou 1 was equipped with fixed solar cells. During this first flight there were also no orbit changes. According to Qi Faren the chief designer of the spacecraft, only 8 of the 13 sub-systems on board the spacecraft were operational. Shenzhou 1 was designed primarily to test the Long March 2F rocket. The only systems and capabilities tested on the spacecraft were the separation of the modules, attitude control, lifting body reentry, the heat shield, and ground recovery.

Shenzhou Details

China Aerospace Science and Technology Corporation

China Aerospace Science and Technology Corporation

(CASC)

Chairman & President: Lei Fanpei Founded: 1999 Successes: 470 Failures: 14 Pending: 8

Agency Type:

The China Aerospace Science and Technology Corporation (CASC) is the main contractor for the Chinese space program. It is state-owned and has a number of subordinate entities which design, develop and manufacture a range of spacecraft, launch vehicles, strategic and tactical missile systems, and ground equipment. It was officially established in July 1999 as part of a Chinese government reform drive, having previously been one part of the former China Aerospace Corporation. Various incarnations of the program date back to 1956.

INFO WIKI

Jiuquan Satellite Launch Center, People's Republic of China

Launch Area 4 (SLS-1 / 921)


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