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

P4
SNPE solid rocket engine. Out of Production. Used on Diamant B launch vehicle. First flight 1970. Diamant BP second stage.

AKA: Diamant BP-2; P-4. Status: Out of Production. Number: 9 . Thrust: 176.50 kN (39,679 lbf). Gross mass: 4,500 kg (9,900 lb). Unfuelled mass: 1,000 kg (2,200 lb). Specific impulse: 273 s. Specific impulse sea level: 240 s. Burn time: 55 s. Height: 2.60 m (8.50 ft). Diameter: 1.50 m (4.90 ft).

Thrust (sl): 155.200 kN (34,890 lbf). Thrust (sl): 15,824 kgf.

Country: France. Launch Vehicles: MSBS M112, MSBS M011, MSBS M012, MSBS M013, Diamant B, MSBS M1, Diamant BP.4. Propellants: Solid. Stages: P4. Agency: SNPE. More at: 11593.



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