Testing of the 650 KLBF LOX/LH2 Low Cost Pintle Engine

37th Joint Propulsion Conference and Exhibit

Volumn , Issue , 2001, Pages

  Gavitt, K R ^a   Mueller, T J ^a  

^a NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION; COSTS; ENGINES; NASA; NOZZLE DESIGN; PROPULSION; SEA LEVEL; SPACE PLATFORMS; TEST FACILITIES; TESTING;

CHAMBER PRESSURE; COMBUSTION EFFICIENCIES; COMBUSTION INSTABILITIES; COOPERATIVE AGREEMENTS; EXPANSION RATIO; LOW ENTHALPIES; SPACE TRANSPORTATIONS; THRUST CHAMBER;

SOFTWARE TESTING;

EID: 85085779171     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-3987     Document Type: Conference Paper

References (4)

1. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 16-19 July 2000.
2. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 16-19 July 2000.
3. "Test Results from a Simple, Low-Cost, Pressure-Fed Liquid Hydrogen/Liquid Oxygen Rocket Combustor"", G. Dressier, F. Stoddard, K. Gavitt and M. Klem, 1993 JANNAF Propulsion Meeting, 15-18 November 1993, CIPA Pub. 602, Vol. II, pp 51-67
4. "JANNAF Rocket Engine Performance Test Data Acquisition and Interpretation Manual", CPIA Publication 245, April 1975