In-situ mars rocket and jet engines burning carbon dioxide

35th Joint Propulsion Conference and Exhibit

Volumn , Issue , 1999, Pages

  Wickman, John H ^a  

^a Wickman Spacecraft and Propulsion Company   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC PRESSURE; CARBON DIOXIDE; COMBUSTION; ENGINES; GAS BURNERS; MAGNESIUM POWDER; MARTIAN SURFACE ANALYSIS; PROPULSION; ROCKETS; TURBOMACHINE BLADES;

AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; CARBON DEPOSITES; COMBUSTION TEST; LOW PRESSURES; MARS AIRPLANES; MARS MISSIONS; THRUST ROCKET ENGINES; TURBINE BLADE;

TURBOJET ENGINES;

EID: 84963828894     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-2409     Document Type: Conference Paper

References (1)

1. PEP Thermochemistry Computer Program, Cruise, D.R., “Theoretical Computations of Equilibrium Composition, Thermodynamic Properties, and Performance Characteristics of Propellant Systems”, NWC TP-6037, April 1979.