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Engine Model: Sergeant. Gross Mass: 42 kg (92 lb). Empty Mass: 21 kg (46 lb). Propellants: Solid. Thrust(vac): 6.660 kN (1,497 lbf). Thrust(sl): 6.073 kN (1,365 lbf). Isp: 235 sec. Isp (sea level): 214 sec. Burn time: 6.00 sec. Diameter: 0.30 m (0.98 ft). Length: 1.00 m (3.20 ft). Chambers: 1. Country: USA. Status: Out of Production. First Flight: 1956. Last Flight: 1961. Flown: 285.

Used in Jupiter C, Juno 2.



Sergeant used on Rocket Stages


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