Monopropellant selection criteria-hydrazine and other options

35th Joint Propulsion Conference and Exhibit

Volumn , Issue , 1999, Pages

  Morgan, Olwen ^a   Meinhardt, Dennis ^a  

^a Primex Aerospace Company   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

HYDRAZINE; MONOPROPELLANTS; PROPULSION; SPACECRAFT;

HIGH RELIABILITY; LOW COSTS; PROPULSION SYSTEM; REDUCED COST; SELECTION CRITERIA; SPACECRAFT APPLICATION; TRADE-STUDY;

SPACECRAFT PROPULSION;

EID: 84963852839     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Schmidt, Eckart W., Hydrazine and Its Derivatives. John Wiley and Sons, 1984.
2. Morrisey, Donald C. “Historical Perspective: Viking Mars Lander Propulsion”. Journal of Propulsion and Power Volume 8 No. 2, March-April 1992, Pages 320-331.
3. Constanza, Robert A., “Simulated Mission Testing of a 0.2 lbf Magellan Monopropellant Thruster”, AIAA Paper 92-3804.
4. Sutton, George P. and Ross, Donald M., Rocket Propulsion Elements. John Wiley and Sons, 1976.
5. Meinhardt, D.S. and Christofferson, S., “Performance and Life Testing of Small HAN Thrusters”. AIAA Paper 99-2881.
6. Urban, M. Gruner, Morrissey, Sneiderman, “Investigation of Propulsion System Requirements for Spartan Lite”. 12th Annual Conference on Small Satellites, SSC98-VIII-5.
7. Whitehead, John C. “Hydrogen Peroxide for Smaller Satellites”. AIAA/USU Conference on Small Satellites, 1998. SSC98-Vm-l.
8. PRIMEX Aerospace Company “Hydrazine Handbook”.
9. McKevitt, F.X., “Design and Development Approach for the Augmented Catalytic Thruster (ACT). AIAA Paper 83-1255.
10. Roberts, C.R., “Life Demonstration Test of an Uprated Augmented Catalytic Thruster”, AIAA Paper 87-0996
11. Smith, R.D., Roberts, C.R., Davies, K., and Vaz, J. Development and Demonstration of a 1.8 kW Hydrazine Arcjet Thruster. AIAA Paper 90-2547.
12. Parker, Morgan, Thunnissen, Dan, Blandino, John, and Ganapathi, G. “The Preliminary Design and Status of a Hydrazine Millinewton Thruster Development”. AIAA-99-2596.
13. Wilson, A.C., and Connors, J. J. “Low Cost Liquid Upper Stage for the Lockheed Launch Vehicle”. AIAA-94-3378.
14. Hearn, H.C., Wilson, A.C., “Evaluation of Dual Mode Orbit Adjust Module for Enhanced LLV Performance”. AIAA-95-2839.
15. Swink, Donald, Morgan, Olwen, and Robinson, John. “Design and Analysis of a Low Cost Reaction Control System for GPS IBP”. AIAA-99-2469.