Mission: Common upper stage engine for Ares I and Ares V. Challenge: Use proven technology from Saturn X-33, RS-68 to develop the highest Isp GG cycle engine in history for 2 missions in record time . Key Features: LOX/LH2 GG cycle, series turbines (2), HIP-bonded MCC, pneumatic ball-sector valves, on-board engine controller, tube-wall regen nozzle/large passively-cooled nozzle extension, TEG boost/cooling . Development Philosophy: proven hardware, aggressive schedule, early risk reduction, requirements-driven.
J-2X Upper Stage Engine: Hardware and Testing 2009
AIAA SPACE 2009 Conference and Exposition ; 2009 ; Pasadena, CA, United States
2009-09-14
Aufsatz (Konferenz)
Keine Angabe
Englisch
J-2X Upper Stage Engine: From Design to Hardware
NTIS | 2010
|J-2X Upper Stage Engine: From Heritage to Hardware
NTIS | 2008
|The J-2X Upper Stage Engine: From Heritage to Hardware
NTRS | 2008
|The J-2X Upper Stage Engine: From Design to Hardware
AIAA | 2010
|The J-2X Upper Stage Engine: From Design to Hardware
NTRS | 2010
|