Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber

32nd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1996, Pages

  Wadel, Mary F ^a   Meyer, Michael L ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION CHAMBERS; COOLANTS; DROPS; EXPLOSIVES; LIQUEFIED GASES; MASS TRANSFER; NASA; PRESSURE DROP; PROPULSION; ROCKET ENGINES; ROCKETS; THERMAL CYCLING; THERMOCOUPLES; WALL FLOW;

COMPUTER ANALYSIS; COOLANT PRESSURE; COOLING CHANNELS; FUEL MASS FLOW RATES; GASEOUS HYDROGEN; HIGH ASPECT RATIO; LIQUID HYDROGENS; ROCKET COMBUSTION CHAMBERS;

ASPECT RATIO;

EID: 84961927540     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Carlile, J.A., Quentmeyer, R.J.: An Experimental Investigation of High-Aspect- Ratio Cooling Passages, 28th Joint Propulsion Conference, 1992, AIAA-92-3154 (Also NASA TM-105679).
2. Wadel, M.F., Quentmeyer, R.J., Meyer, M.L.: A Rocket Engine Design for Validating the High Aspect Ratio Cooling Channel Concept, NASA Conference Publication 3282, Vol. 2, pp. 145-150.
3. Naraghi, M.H.N.: User's Manual, RTE - A Computer Code for Three-Dimensional Rocket Thermal Evaluation, Manhattan College, Riverdale, NY, September 1993, under NASA grant NAG 3-892.
4. Nickerson, G.R., Coats, D.E., Dang, A.L., Dunn, S.S., Kehtarnavaz, H.: Two- Dimensional Kinetics (TDK) Nozzle Performance Computer Program, NAS8- 36863, March 1989.
5. Muss, J.A., Nguyen, TV., Johnson, C.W.: User's Manual for Rocket Combustor Interactive Design (ROCCID) and Analysis Computer Program, NASA Contractor Report 187109, Contract NAS3-25556, May 1991.