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...
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Rocketdyne J-2
Spaceflight
Status:
Used in rocket stages:
| Rocket | Stage Number | Thrust (newtons) | Burn Time (seconds) | Fuels |
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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:
Fuel:
Oxidizer:
Oxidizer/fuel ratio:
- 5.5
Expansion ratio:
- 27.5
Chamber pressure:
- 30 bar (440 psi )
Number of chambers:
- 1