Difference between revisions of "J-2X (Engine)"
Jump to navigation
Jump to search
m |
(Added category.) |
||
| (One intermediate revision by the same user not shown) | |||
| Line 10: | Line 10: | ||
*[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)