Modeling a hydrogen peroxide gas generator for rockets

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

Volumn , Issue , 2000, Pages

  Chiappetta, L M ^a   Spadaccini, L J ^a   Huang, H ^a   Watkins, W ^b   Crocker, A M ^b  

^a UNITED TECHNOLOGIES RESEARCH CENTER   (United States)

^b PRATT AND WHITNEY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

GAS GENERATORS; HYDROGEN PEROXIDE; NOZZLE DESIGN; OXIDATION; PEROXIDES; POROUS MATERIALS; PROPULSION; ROCKETS;

CATALYTIC DECOMPOSITION; COMPUTATIONAL FLUID DYNAMICS CODES; FLOW CHARAC-TERISTICS; GENERIC DESIGN; HYDROGEN PEROXIDE DECOMPOSITION; HYDROGEN PEROXIDE GAS; ROCKET PROPULSION; THREE DIMENSIONAL FLOW SIMULATION;

COMPUTATIONAL FLUID DYNAMICS;

EID: 85088720330     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-3223     Document Type: Conference Paper

References (4)

1. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Los Angeles, CA., June 20-24, 1999
2. Schumb, W. C., Satterfield, C. N., and Wentworth, R. L., Hydrogen Peroxide, Reinhold Publishing Corporation, New York, N. Y., 1955
3. Runckel, J. F., C. M. Willis and L. B. Sailers, "Investigation of Catalyst Beds for 98-percent Concentration Hydrogen Peroxide", NASA TN D 1808, June 1963.
4. Schmauch, G. E. and B. Bailey: "Oxygen Supply Systems for Manned Space Enclosures", Air Products and Chemicals, Inc., Report No. AMRL-TR-66.169, 1966