Difference between revisions of "J-2X (Engine)"
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| − | The '''J-2X''' is a modern [[ | + | The '''J-2X''' is a modern [[gas-generator cycle]], [[bi-propellant]] [[rocket engine]], planned for use in the [[Ares I]] and [[Ares V]] [[launch vehicles]]. It consumes [[liquid hydrogen]] and [[liquid oxygen]]. It has its origin in the [[J-2 (Engine)|J-2]] rocket engines used by the [[Saturn Ib]] and [[Saturn V]] launchers. It is produced by [[Pratt & Whitney Rocketdyne]]. |
| − | ==Differences to the J-2== | + | <!-- ==Differences to the J-2== |
[[Image:J2X_schematic.gif|thumb|right|Schematic of the J-2X]] | [[Image:J2X_schematic.gif|thumb|right|Schematic of the J-2X]] | ||
| − | While the J-2 was a [[gas-generator cycle]] or open cycle rocket engine, the '''J-2X''' uses so called [[tap-off cycle]] for powering its [[turbopumps]]. In such a cycle, a small part of the hot exhaust gases from the [[combustion chamber]] is used for powering the two turbopump assemblies. these turbopumps are connected in series with a hot-gas duct. After passing the oxidizer turbopump, the hot gases are directed into the nozzle exhaust stream. | + | While the J-2 was a [[gas-generator cycle]] or open cycle rocket engine, the '''J-2X''' uses so called [[tap-off cycle]] for powering its [[turbopumps]]. In such a cycle, a small part of the hot exhaust gases from the [[combustion chamber]] is used for powering the two turbopump assemblies. these turbopumps are connected in series with a hot-gas duct. After passing the oxidizer turbopump, the hot gases are directed into the nozzle exhaust stream. --> |
==References== | ==References== | ||
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*[http://www.nasa.gov/pdf/187393main_j-2x_fact_sheet.pdf J-2X fact sheet from NASA (2.9 MB)] | *[http://www.nasa.gov/pdf/187393main_j-2x_fact_sheet.pdf J-2X fact sheet from NASA (2.9 MB)] | ||
| − | [[Category: | + | [[Category: Articles]] |
| + | [[Category:Rocket engines]] | ||
{{Stub}} | {{Stub}} | ||
Latest revision as of 12:12, 14 October 2022
The J-2X is a modern gas-generator cycle, bi-propellant rocket engine, planned for use in the Ares I and Ares V launch vehicles. It consumes liquid hydrogen and liquid oxygen. It has its origin in the J-2 rocket engines used by the Saturn Ib and Saturn V launchers. It is produced by Pratt & Whitney Rocketdyne.
References[edit]
- Pratt & Whitney Rocketdyne Awarded $1.2 Billion NASA Contract for J-2X Ares Rocket Engine
- J-2S on astronautix.com
- J-2X fact sheet from NASA (2.9 MB)