S-3B engine Credit: USAF |
Status: First flight 1958. Number: 10 . Thrust: 758.70 kN (170,563 lbf). Unfuelled mass: 725 kg (1,598 lb). Specific impulse: 282 s. Specific impulse sea level: 248 s. Burn time: 182 s. Diameter: 2.67 m (8.75 ft).
Thrust (sl): 667.200 kN (149,993 lbf). Thrust (sl): 68,039 kgf. Engine: 725 kg (1,598 lb). Chamber Pressure: 39.50 bar. Area Ratio: 8. Thrust to Weight Ratio: 106.713103448276. Coefficient of Thrust vacuum: 1.71921743620711. Coefficient of Thrust sea level: 1.51668579063749.