TRW LCPE 650 klbf LOX/LH2 test results

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Gavitt, K ^a   Mueller, T ^a   Wang, T ^a   Thorn, H ^a   Murphy, C ^a   Weede, J ^a  

^a NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ENGINES; FLAMMABILITY TESTING; HARDWARE; LAUNCH VEHICLES; NASA; PROPULSION; SPACE PLATFORMS;

COOPERATIVE AGREEMENTS; DESIGN FEATURES; LOW COSTS; PINTLE ENGINE; SPACE CENTERS; SPACE TRANSPORTATIONS; TEST PROGRAM; VEHICLE PROPULSION;

SOFTWARE TESTING;

EID: 69249083466     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (2)

1. "TRW Pintle Engine Heritage and Performance Characteristics", G. A. Dressier and J. M. Bauer, AIAA2000- 3871, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 16-19 July 2000.
2. "Test Results from a Simple, Low-Cost, Pressure-Fed Liquid Hydrogen/Liquid Oxygen Rocket Combustor", G. Dressier, F. Stoddard, K. Gavittand M. Klem, 1993 JANNAF Propulsion Meeting, 15-18 November 1993, CIPA Pub. 602, Vol. II, pp51-67