Considerations in designing the air-breathing engines for a spaceplane acceleration mission

Space Plane and Hypersonic Systems and Technology Conference

Volumn , Issue , 1996, Pages

  Sippel, Martin ^a   Pohl, Martin ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; AIR ENGINES; AIR INTAKES; BYPASS RATIO; ENGINES; NOZZLE DESIGN; PROPULSION; ROCKETS; SPACECRAFT; SPACECRAFT PROPULSION; SUPERSONIC AERODYNAMICS; SUPERSONIC AIRCRAFT;

AIR BREATHING ENGINES; ANALYTICAL DESIGN; ENGINE PERFORMANCE CALCULATION; MULTI DIMENSIONAL; PRELIMINARY DESIGN; PROPULSION SYSTEM; THRUST-TO-WEIGHT RATIO; TURBINE ENTRY TEMPERATURE;

FIGHTER AIRCRAFT;

EID: 84983130809     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

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