Shenzhou 1

Shenzhou 1

Return capsule of Shenzhou 1 displayed at China Science and Technology Museum
Mission type	Test flight
COSPAR ID	1999-061A
SATCAT no.	25956
Mission duration	21 hours, 11 minutes
Orbits completed	14
Spacecraft properties
Spacecraft type	Shenzhou
Launch mass	7600 kg
Start of mission
Launch date	19 November 1999, 22:30 UTC
Rocket	Long March 2F
Launch site	Jiuquan, LA-4/SLS-1
Contractor	China Academy of Launch Vehicle Technology (CALT)
End of mission
Landing date	20 November 1999, 19:41 UTC
Landing site	Inner Mongolia 41°N 105°E / 41°N 105°E / 41; 105
Orbital parameters
Reference system	Geocentric orbit
Regime	Low Earth orbit
Perigee altitude	195 km
Apogee altitude	315 km
Inclination	42.6°
Period	89.6 minutes
Shenzhou missions Shenzhou 2 →

Shenzhou 1 (simplified Chinese: 神舟一号; traditional Chinese: 神舟一號; pinyin: Shénzhōu Yīhào) launched on 19 November 1999, was the first uncrewed launch of the Shenzhou spacecraft. The spacecraft used was not equipped with a life support system or an emergency escape system. After orbiting the Earth 14 times, the command for retrofire was sent by the Yuan Wang 3 tracking ship off the coast of Namibia at 18:49 UTC. After a successful reentry it landed about 415 kilometres (258 mi) east of its launch pad and 110 kilometres (68 mi) north-west of Wuhai, Inner Mongolia.

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.

The spacecraft is thought to have carried 100 kilograms (220 lb) of seeds to investigate the effects on them of the space environment. It is also thought that the front of the Orbital module was equipped with a dummy ELINT package, with Shenzhou 2 onwards equipped with fully functional models.

It was announced in June 1999 that the flight would take place in October of that year. At about the same time images were released on a Chinese military internet forum of the Long March 2F launcher and the Vehicle Assembly Building that would be used. After a reported^[who?] propellant explosion at the Jiuquan Satellite Launch Center (though the explosion was denied by Chinese officials) the launch was pushed back.

Mission parameters

• NSSDC ID: 1999-061A
• Mass: 7600 kg
• Perigee: 195 km
• Apogee: 315 km
• Inclination: 42.6°
• Period: 89.6 minutes

See also

• Chinese space program
• Tiangong program
• Shenzhou spacecraft
• Long March rocket
• Jiuquan Satellite Launch Center

References

• "Shenzhou". Encyclopedia Astronautica. Archived from the original on 13 October 2005. Retrieved 13 December 2010.

• "Shenzhou Unmanned Spaceflight Mission". Chinese Defence Today. Archived from the original on 11 April 2005. Retrieved 13 December 2010.

• Kang Lim, Benjamin (21 November 1999). "China Launches Its First Unpiloted Spacecraft and Joins Exclusive Club". Space.com. Reuters. Retrieved 13 December 2010.

• Wade, Mark (2 October 2003). "Shenzhou — Divine Military Vessel". SpaceDaily. Retrieved 13 December 2010.

• "Details About Courses Running up to 1st Manned Spaceflight". Xinhua News Agency. 16 October 2003. Retrieved 13 December 2010.

This page was last edited on 14 July 2023, at 13:00