M33

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Engine Model: M33-20-4. Designer: Thiokol. Gross Mass: 3,852 kg (8,492 lb). Empty Mass: 535 kg (1,179 lb). Propellants: Solid. Thrust(vac): 286.000 kN (64,295 lbf). Thrust(sl): 268.600 kN (60,384 lbf). Isp: 247 sec. Isp (sea level): 232 sec. Burn time: 27 sec. Diameter: 0.79 m (2.59 ft). Length: 5.92 m (19.42 ft). Chambers: 1. Country: USA. First Flight: 1960. Last Flight: 1971. Flown: 141. M33 used on Rocket Stages Used on stage: Castor. on launch vehicle: ARPAT. Used on stage: Castor. on launch vehicle: Athena RTV. Used on stage: Castor. on launch vehicle: Castor-Orbus. Used on stage: Castor. on launch vehicle: Delta. Used on stage: Castor. on launch vehicle: DOT. Used on stage: Castor. on launch vehicle: Little Joe. Used on stage: Castor. on launch vehicle: Polaris. Used on stage: Castor. on launch vehicle: RAM. Used on stage: Castor. on launch vehicle: Scout. Used on stage: Castor. on launch vehicle: Sergeant. Used on stage: Castor. on launch vehicle: Strypi. Used on stage: Castor. on launch vehicle: Super Chief. Used on stage: Castor. on launch vehicle: Trailblazer. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.