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Also known as Rocket System 68

The RS-68 (Rocket System-68) was a liquid-fuel rocket engine that used liquid hydrogen (LH2) and liquid oxygen (LOX) as propellants in a gas-generator cycle. It was the largest hydrogen-fueled rocket engine ever flown.

Key facts

Rocket engine.image
RS-68 rocket engine test.jpg
Rocket engine.caption
An RS-68 engine undergoing hot-fire testing at NASA's Stennis Space Center during its developmental phase.
Rocket engine.name
RS-68
Rocket engine.purpose
First stage engine
Rocket engine.associated
Delta IVDelta IV Heavy
Rocket engine.country_of_origin
United States
Rocket engine.thrust_to_weight
RS-68: 45.3:1RS-68A: 47.4:1
Rocket engine.specific_impulse_vacuum
RS-68: RS-68A:
Rocket engine.dry_weight
RS-68: RS-68A:
Rocket engine.designer
Rocketdyne
Rocket engine.type
liquid
Rocket engine.status
Retired
Rocket engine.oxidiser
LOX
Rocket engine.cycle
Gas-generator
Rocket engine.nozzle_ratio
21.5:1
Rocket engine.thrust(SL)
RS-68: RS-68A:

via Wikipedia infobox

Wikidata facts

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RS-68 rocket engine test.jpg
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Commons category
RS-68 (rocket engine)
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Article

7 sections
Contents
  • Design and development
  • Proposed uses
  • Human-rating
  • Variants
  • See also
  • References
  • External links

The RS-68 (Rocket System-68) was a liquid-fuel rocket engine that used liquid hydrogen (LH2) and liquid oxygen (LOX) as propellants in a gas-generator cycle. It was the largest hydrogen-fueled rocket engine ever flown.

Designed and manufactured in the United States by Rocketdyne (later Pratt & Whitney Rocketdyne and Aerojet Rocketdyne). Development started in the 1990s with the goal of producing a simpler, less costly, heavy-lift engine for the Delta IV launch system. Two versions of the engine have been produced: the original RS-68 and the improved RS-68A. A third version, the RS-68B, was planned for the National Aeronautics and Space Administration's (NASA) Ares V rocket before the cancellation of the rocket and the Constellation Program in 2010.

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