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Mammouth

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Mammouth
French solid rocket engine. 1900 kg 'Plastolite' propellant. Empty mass estimated. Originally developed as the booster for the SSBT missile. Used on Agate launch vehicle. First flight 1961.
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AKA: NA801. Thrust: 190.00 kN (42,710 lbf). Gross mass: 2,900 kg (6,300 lb). Unfuelled mass: 1,000 kg (2,200 lb). Specific impulse: 180 s. Burn time: 18 s.

Subtopics
NA 802 Soleil C SEREB solid rocket engine.
NA 803 Soleil SEREB solid rocket engine.
Country: France. Launch Vehicles: Agate. Propellants: Solid.
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