Difference between revisions of "J-2X (Engine)"

From OrbiterWiki
Jump to navigation Jump to search
m
(Changed category.)
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:rocket engines]]
+
[[Category:Rocket engines]]
 
{{Stub}}
 
{{Stub}}

Revision as of 03:32, 11 May 2021

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

This article is a stub. You can help Orbiterwiki by expanding it.