Design and development testing of the TR108 - A 30KLbfthrust-class hydrogen peroxide/hydrocarbon pump-fed engine

41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2005, Pages

  Kim, Paul Y ^a,b   Majamaki, Annik ^a,b   Papesh, Charles ^a,b   Schneider, Darrick ^a,b   Thomson, Matt ^a,c   Weinstock, Vladimir D ^a,b  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b M S 140 2134C

^c M/S 140/2121D ^*

Author keywords

[No Author keywords available]

Indexed keywords

ENGINES; GAS GENERATORS; HYDROGEN FUELS; HYDROGEN PEROXIDE; OXIDATION; PEROXIDES; PROPULSION; TURBINE PUMPS; WELL TESTING;

COMPONENT DESIGN; DESIGN AND DEVELOPMENT; DEVELOPMENT PROGRAMS; ENGINE CONFIGURATION; FULLY INTEGRATED; MISSILE DEFENSE AGENCY; NORTHROP GRUMMAN; OPERATING CONDITION;

SOFTWARE TESTING;

EID: 77957834364     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-3566     Document Type: Conference Paper

References (3)

1. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, July 2000.
2. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, July 2000.
3. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, AL, July 2003.