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NOTS-4
NOTS solid rocket engine. Out of production. Used on Caleb launch vehicle. First flight 1960. Caleb fourth stage.

AKA: Caleb-4. Status: Out of production. Number: 7 . Thrust: 700 N (150 lbf). Gross mass: 5.00 kg (11.00 lb). Unfuelled mass: 1.00 kg (2.20 lb). Specific impulse: 250 s. Specific impulse sea level: 204 s. Burn time: 3.00 s.

Thrust (sl): 576 N (130 lbf). Thrust (sl): 59 kgf.



Country: USA. Launch Vehicles: Caleb. Propellants: Solid. Stages: NOTS-4. Agency: NOTS.

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