Second Stage

 

 

Second Stage – S-II

 

Length Diameter Empty mass

Gross mass

Engines

Thrust Specific Impulse Burn Time Fuel 81.5 feet (24.8 m) 33.0 feet (10.1 m)

88,400 pounds (40,100 kg)

1,093,900 pounds (496,200 kg) 5 Rocketdyne J-2 1,000,000 lbf (4,400 kN) 421 seconds (4.13 km/s) 360 seconds LH2/LOX

 

 SATURN V ROCKET FROM ENGINE TO FRONT VIEW : JOHNSON SPACE CENTER HOUSTON TEXAS

 SATURN V ROCKET STAGE TWO : JOHNSON SPACE CENTER – HOUSTON TEXAS

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