Altitude Testing of the J2-X engine at 100,000 feet (start capability). Chemical Steam Generation for providing vacuum. Project Started Mar 07. Test Stand Activation around Late 2010. J-2X Testing around early 2011.
Altitude Testing of Large Liquid Propellant Engines
2008
31 pages
Report
Keine Angabe
Englisch
Altitude Testing of Large Liquid Propellant Engines
NTRS | 2008
|Altitude Testing of Large Liquid Propellant Engines
AIAA | 2008
|Altitude Testing of Large Liquid Propellant Engines
NTRS | 2010
|Altitude start capability of existing large liquid propellant rocket engines
Engineering Index Backfile | 1960
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