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P4

Engine · France

Original archive entry. The text, images and links below are kept as they were written.

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

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

Country
France
Propellants
Solid
Stages
P4
Agency
SNPE