Design and testing of non-toxic RCS thrusters for second generation reusable launch vehicles

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2003, Pages

  Calvignac, Jacky ^a   Dang, Lisa ^a   Tramel, Terri L ^b   Paseur, Lila ^b  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b NASA MARSHALL SPACE FLIGHT CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTION EFFICIENCIES; DESIGN APPROACHES; ENABLING TECHNOLOGIES; INJECTION TEMPERATURE; NORTHROP GRUMMAN SPACE TECHNOLOGIES; OPERATING CONDITION; REACTION CONTROL; SECOND GENERATION REUSABLE LAUNCH VEHICLES;

COMBUSTION CHAMBERS; DESIGN; ENGINES; LIQUEFIED GASES; NASA; PROPULSION; SEA LEVEL; SPACE FLIGHT;

DUCTS;

EID: 84897585204     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (1)

1. Test Report-DRD RCST. 951-DE-020-LH2, Revision A; dated September 20, 2002.