The design and development of the MR-510 Arcjet power conditioning unit

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Fisher, J R ^a   Meyer, S D ^a  

^a Primex Aerospace Company   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

NITROGEN COMPOUNDS; PROPULSION; SATELLITES; TOPOLOGY;

AEROSPACE COMPANY; ARC JET THRUSTER; DESIGN AND DEVELOPMENT; LOCKHEED MARTIN; ON-ORBIT PERFORMANCE; POWER CONDITIONING UNIT; QUALIFICATION TEST; STATION KEEPING;

ORBITS;

EID: 84858497988     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-3630     Document Type: Conference Paper

References (6)

1. Smith, R.D., Yano, S.E., Armbruster, K., Roberts, C.R., Lichtin, D.A. and Beck, J.W., “Flight Qualification of a 1.8 kW Hydrazine Arcjet System”, AIAA-93-007, September, 1993.
2. Skelly, P.T., Fisher, J.R., Golden, C.M., “Power Conditioning Unit for Low-Power Arcjet Flight Application”, AIAA-92-3529, July, 1992.
3. Smith, R.D., Roberts, C.R., Aadland, R.S., Lichtin, D.A., Davies, K.A., “Flight Qualification of the 1.8 kW MR-509 Hydrazine Arcjet System”, IEPC-97-081, 25th IEPC, August, 1997.
4. Smith, R.D., Aadland, R.S., Roberts, C.R., Lichtin, D.A., “Flight Qualification of the 2.2 kW MR-510 Hydrazine Arcjet System”, IEPC-97-082, 25th IEPC, August, 1997.
5. U.S. Patent No. 5,605,039, Parallel Arcjet Starter System, February 25, 1997.
6. Nagle, S.M., “A System for the Test of a Space Electronics Device”, IEEE Autotestcon ‘96, September, 1996.