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searching for Rocketdyne J-2 4 found (25 total)

Saturn INT-21 (310 words) [view diff] exact match in snippet view article find links to article

time 150 seconds Propellant RP-1 / LOX Second stage S-II Engines 5 Rocketdyne J-2 Thrust 5 MN (1,100,000 lbf) Burn time 360 seconds Propellant LH2 / LOX

Jarvis (rocket) (1,031 words) [view diff] exact match in snippet view article

by the Saturn V's first stage. The second stage would use a single Rocketdyne J-2 LOX/liquid hydrogen (LH2) engine, while the third stage was intended

Saturn C-8 (449 words) [view diff] exact match in snippet view article find links to article

345 lb (13,311 kg) Gross mass 264,370 lb (119,920 kg) Powered by 1 Rocketdyne J-2 Maximum thrust 220,000 lbf (1,000 kN) Specific impulse 425 s (4.17 km/s)

Saturn C-3 (1,922 words) [view diff] exact match in snippet view article find links to article

pounds (24,938 kg) Gross mass 449,840 pounds (204,040 kg) Powered by 4 Rocketdyne J-2 Maximum thrust 800,000 pounds-force (3,600 kN) Specific impulse 300