Rocketdyne J-2

Rocketdyne's J-2 was America's largest production liquid hydrogen fueled rocket engine before the Space Shuttle main engines (SSME), and is being revived in support of NASA's return to the Moon. The J-2 was a major component of the Saturn V rocket. Five J-2 engines were used on the S-II, the second stage of the Saturn V. One J-2 engine was used on the S-IVB, the third stage of the Saturn V, and the second stage of the Saturn IB. There were propos... more

Spaceflight

Status:

Used in rocket stages:

Rocket Stage Number Thrust (newtons) Burn Time (seconds) Fuels
  • 3
  • 1,000,000 N (7233014 pdl )
  • 2
  • 5,000,000 N (36165070 pdl )
  • 2 min 30 s
  • 2
  • 5,000,000 N (36165070 pdl )
  • 6 min
View entire collection »

Designed by:

Diameter:

  • 2.01 m (6.59 ft )

Height:

  • 3.38 m (11.1 ft )

Thrust (vacuum):

  • 890,000 N (6437380 pdl )

Isp (vacuum):

  • 6 min 58 s

Dry mass:

  • 1,579 kg (3481 lb )

Wet mass:

  • 1,637 kg (3609 lb )

Engine cycle:

Oxidizer:

Oxidizer/fuel ratio:

  • 5.5

Expansion ratio:

  • 27.5

Chamber pressure:

  • 30 bar (440 psi )

Number of chambers:

  • 1
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