The Wayback Machine - https://web.archive.org/web/20170517221445/http://www.astronautix.com:80/c/changchengstage1.html
Chang Cheng stage 1

Encyclopedia Astronautica
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Chang Cheng stage 1
Part of Chang Cheng 1 Family
LOx/LH2 propellant rocket stage. All characteristics except dimensions estimated, on assumption that stage used same propulsion systems as Shanghai upper stage.
See More

AKA: Chang Cheng 1. Status: Design 1988. Thrust: 490.00 kN (110,150 lbf). Gross mass: 57,000 kg (125,000 lb). Unfuelled mass: 30,000 kg (66,000 lb). Specific impulse: 230 s. Burn time: 430 s. Height: 24.00 m (78.00 ft). Diameter: 4.50 m (14.70 ft). Span: 17.00 m (55.00 ft).

Family: Chinese Manned Spacecraft, Spaceplane. Country: China. Launch Vehicles: Chang Cheng 1. Propellants: Lox/LH2. Agency: SAST.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
� 1997-2016 Mark Wade - Contact
� / Conditions for Use