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

T-7A Booster
Fourth Academy solid rocket engine. T-7 sounding rocket. Out of Production. China's first flight solid rocket. First flight 1965. Polysulfide binder with aluminum binder fuel in case of high strength steel with a graphite throat insert.

AKA: Sounding Rocket Motor; T-7A-S2-0. Status: Out of Production. Date: 1962-1966. Thrust: 46.00 kN (10,341 lbf). Gross mass: 150 kg (330 lb). Unfuelled mass: 33 kg (72 lb). Specific impulse: 209 s. Burn time: 7.50 s. Height: 1.82 m (5.98 ft). Diameter: 0.29 m (0.94 ft).

Fourth Academy solid rocket engine. T-7 sounding rocket. Out of Production. China's first flight solid rocket. First flight 1965. Polysulfide binder with aluminum binder fuel in case of high strength steel with a graphite throat insert. T-7A-S2 zero stage.

Propellant Formulation: Polysulfide.

Country: China. Launch Vehicles: T-7. Propellants: Solid. Stages: T-7 booster. 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