SEPR 737 (original) (raw)

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SEPR 737

ONERA solid rocket engine. VE10A Aigle first stage.

AKA: VE10A Aigle-1. Status: Retired 1964. Thrust: 75.00 kN (16,860 lbf). Gross mass: 900 kg (1,980 lb). Unfuelled mass: 246 kg (542 lb). Burn time: 16 s. Height: 3.00 m (9.80 ft). Diameter: 0.56 m (1.83 ft).

Country: France. Launch Vehicles: VE10 Aigle, VE10A Aigle. Propellants: Solid. Stages: SEPR 737. Agency: ONERA.

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