Modeling hypergolic ignition in the army's impinging stream vortex engine including injection throttling

Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference

Volumn 5, Issue , 2007, Pages 4260-4278

  Nusca, Michael J ^a,c   Mathis, Nathan P ^b,c,d   Michaels, R Scott ^b,c,d  

^a U S ARMY RESEARCH LABORATORY   (United States)

^b US Army Aviation and Missile Command   (United States)

^c AIAA   (United States)

^d AMSRD AMR PS PT

Author keywords

[No Author keywords available]

Indexed keywords

IGNITION; MATHEMATICAL MODELS; MISSILES; PROPULSION;

HYPERGOLIC GEL PROPELLANTS; HYPERGOLIC IGNITION; INJECTION THROTTLING;

ENGINES;

EID: 36749082397     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-5443     Document Type: Conference Paper

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