TRW 40 klbf LOX/RP-1 low cost pintle engine test results

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

Volumn , Issue , 2000, Pages

  Mueller, Tom ^a   Dressier, Gordon ^a  

^a NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOMBS (ORDNANCE); NASA; PROPULSION; ROCKET ENGINES;

COMBUSTION EFFICIENCIES; HEAVY-LIFT LAUNCH VEHICLES; LOW COSTS; LOX/KEROSENE; PINTLE ENGINE; SINGLE ELEMENT; SPACE EXPLORATIONS; THRUST LEVELS;

COST REDUCTION;

EID: 84896468294     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Dressier, G. A., Stoddard, F. J., Gavitt, K. R., and Kiem, M., "Test Results from a Simple, Low-Cost, Pressure-Fed Liquid Hydrogen/Liquid Oxygen Racket Combustor," JANNAF Propulsion Meeting, Monterey, CA., November 15-18,1993,
2. nd JANNAF Combustion Subcommittee Meeting, Huntsville, AL, 23-37 October, 1995.
3. nd JANNAF Combustion Subcommittee Meeting, Huntsville, AL., 23-37 October, 1995.
4. Gavitt, K. R., Hardgrove, J., Mueller, T., Weede, J., Johnson, C., and Saville, M., "TRWs Ultra Low Cost LOX/LH2 Booster Liquid Rocket Engine," AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Seattle, WA., July, 1997.
5. G. A. Repas, G. A., "Hydrogen-Oxygen Torch Igniter," NASA TM-106493, NASA Lewis Research Center, Cleveland OH, March 1994.