High performance 400N MMH/NTO bipropellant engine for apogee boost maneuvers

35th Joint Propulsion Conference and Exhibit

Volumn , Issue , 1999, Pages

  Schulte, G ^a  

^a DAIMLER AG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

C (PROGRAMMING LANGUAGE); ENGINES; ORBITS; PLATINUM ALLOYS; PROPELLANTS; PROPULSION; SOFTWARE TESTING;

ACCEPTANCE TESTING; BIPROPELLANT ENGINES; DAIMLER-CHRYSLER; DESIGN MODIFICATIONS; INLET TEMPERATURE; PERFORMANCE TARGETS; QUALIFICATION TEST; STABILITY TESTING;

ACCEPTANCE TESTS;

EID: 84963865062     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-2466     Document Type: Conference Paper

References (7)

1. Biaglow, J.A., "High Temperature Rhenium Material Properties", AIAA Paper 98-3354, July 1998.
2. Reed, B.D., "Rocket Screening of Iridi um/Rhenium Chambers", AIAA.Paper 98-3355, July 1998.
3. Chazen, M., Sicher, D., "High Performance Bipropellant Engine", AIAA Paper 983356, July 1998.
4. Wood, R.S., "Experiences with High Tempe rature Materials for small Thrusters", AIAA Paper 93-1962, June 1993.
5. Driscoll, R.J., Yager, J., Roy, M.J., Kammerer, H.G., "Development Tests ON A 5-LBF Bipropellant Thruster and Using A Platinum/Rhodium, Thrust Chamber", AIAA Paper 98-3357, July 1998.
6. Schwende, M.A., Schulte, G., Dargies, E., Gotzig, U., Scharli-Weinert, E., "New Generation of Low- Thrust Bipropellant Engines in, Qualification Process", AIAA and Paper 93-2120 June 1993.
7. Gotzig,U., Schulte, G., Dargies, E., Scharli-Weinert, E. and Schwende, M.A., "Performance Behaviour and Status of New Generation Thruster Family for Spacecraft Propulsion", International Conference Spacecraft Propulsion, Toulouse Labege-France, Nov. 1994.