![]() 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 Perigee Orbit Transfer Motor Status: In Production. Date: Late 1980's. Thrust: 222.84 kN (50,096 lbf). Gross mass: 4,635 kg (10,218 lb). Unfuelled mass: 496 kg (1,093 lb). Specific impulse: 280 s. Burn time: 65 s. Height: 2.89 m (9.49 ft). Diameter: 1.40 m (4.60 ft). Total impulse 11,360 kN-s over 65.2 seconds.
Propellant Formulation: HTPB.
Country: China. Launch Vehicles: Chang Zheng 2E. Propellants: Solid. Agency: Fourth Academy. Bibliography: 544. 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 |