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NOTS-1
NOTS solid rocket engine. Out of production. Used on Caleb launch vehicle. First flight 1960.

Status: Out of production. Number: 7 . Thrust: 53.40 kN (12,005 lbf). Gross mass: 1,033 kg (2,277 lb). Unfuelled mass: 194 kg (427 lb). Specific impulse: 204 s. Specific impulse sea level: 204 s. Burn time: 34 s. Diameter: 0.60 m (1.96 ft).

Thrust (sl): 53.400 kN (12,005 lbf). Thrust (sl): 5,441 kgf.



Country: USA. Launch Vehicles: Caleb. Propellants: Solid. Stages: NOTS-1. Agency: NOTS.

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