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
26th AIAA Aerodynamic Measurement Technology and Testing Conference Development of Test Facilities Session ; 2008 ; Seattle, WA, United States
2008-06-23
Conference paper
No indication
English
Altitude Testing of Large Liquid Propellant Engines
NTIS | 2008
|Altitude Testing of Large Liquid Propellant Engines
AIAA | 2008
|Altitude Testing of Large Liquid Propellant Engines
NTRS | 2010
|Altitude Testing of Large Liquid Propellant Engines
British Library Conference Proceedings | 2008
|