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-3A-1
Part of CZ-2-1 stage series
N2O4/UDMH propellant rocket stage. .

AKA: L-180. Status: Development ended 1997. Thrust: 3,265.14 kN (734,033 lbf). Gross mass: 179,000 kg (394,000 lb). Unfuelled mass: 9,000 kg (19,800 lb). Specific impulse: 289 s. Specific impulse sea level: 259 s. Burn time: 155 s. Height: 23.08 m (75.72 ft). Diameter: 3.35 m (10.99 ft). Span: 7.00 m (22.90 ft).

Cost $ : 6.000 million. No Engines: 4.



Country: China. Engines: YF-20B. Launch Vehicles: Chang Zheng 3A, Chang Zheng 3B, Chang Zheng 3C. 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