Shenzhou (spacecraft)

Shenzhou
A Shenzhou spacecraft undergoing ground testing without solar panels
ManufacturerChina Academy of Space Technology
Country of origin China
OperatorChina Manned Space Agency
ApplicationsCrewed spaceflight
Specifications
Launch mass8,100 kg (17,900 lb)[1]
Crew capacity3
Dimensions9.25 m × 2.8 m (30.3 ft × 9.2 ft)
VolumeTotal: 14.8 m3 (520 cu ft)[1]
Habitable: 7 m3 (250 cu ft)
RegimeLow Earth
Design lifeUp to 183 days (docked at the Tiangong space station)
Production
StatusIn service
On order1
Built18
Launched18
Operational1
Maiden launch

Shenzhou (Chinese: 神舟; pinyin: Shénzhōu, /ˈʃɛnˈ/;[2] see § Etymology) is a Chinese spacecraft developed for the nation's crewed space program. Its design was based on Russia's Soyuz, but larger and modernized, Shenzhou is a single-use vehicle composed of three modules. The descent module houses the crew during launch and reentry. The orbital module provides additional living space and storage during orbit but is jettisoned before reentry. The service module, responsible for propulsion and power, is also discarded prior to reentry. For added safety and aerodynamics, the spacecraft is encased within a fairing with a launch escape system during liftoff.

Its maiden uncrewed flight, Shenzhou 1, was on 19 November 1999, with the first crewed mission, Shenzhou 5, taking flight on 15 October 2003. It is slated for replacement by the next-generation Mengzhou, currently in development, with a two module configuration that resembles Western spacecraft like Apollo and Dragon.

  1. ^ a b 朱光辰 (2022). "我国载人航天器总体构型技术发展". 航天器工程. 第31卷 (第6期): 47.
  2. ^ "Shenzhou pronunciation". Dictionary.com. Retrieved 25 April 2015.