CZ-2E(A)-0 (original) (raw)


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


CZ-2E(A)-0


Part of CZ-2-0 stage series


N2O4/UDMH propellant rocket stage. .

Status: Design 2000. Thrust: 1,632.80 kN (367,068 lbf). Gross mass: 80,000 kg (176,000 lb). Unfuelled mass: 8,000 kg (17,600 lb). Specific impulse: 291 s. Specific impulse sea level: 261 s. Burn time: 125 s. Height: 27.00 m (88.00 ft). Diameter: 2.25 m (7.38 ft). Span: 2.26 m (7.41 ft).

No Engines: 2.



Country: China. Engines: YF-20B. Launch Vehicles: Chang Zheng 2E(A). Propellants: N2O4/UDMH.



Back to top of page


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


© 1997-2019 Mark Wade - Contact
© / Conditions for Use