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| Content Provider | IEEE Xplore Digital Library |
|---|---|
| Author | Das, R.S.L. Krauthamer, S. Frisbee, R.H. |
| Copyright Year | 1996 |
| Description | Author affiliation: Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA (Das, R.S.L.) |
| Abstract | The power requirement of vehicles designed to transport cargo supporting a piloted expedition to Mars is in the range of megawatts. Therefore, it is imperative that the megawatt class power processing unit designed for high-power nuclear electric propulsion vehicles using turboalternators and advanced magnetoplasmadynamic (MPD) thrusters should be such that the overall system efficiency is as high as possible with minimum system specific mass. This paper examines the use of cryogenic power conditioning subsystems to achieve that goal since they have very high efficiency. In the past, cryogenic power conditioning have shown complexity of design and implementation and were costly and somewhat uncertain. With recent advances in materials, devices used in power conversion and cooling methods, further improvements in efficiency and specific mass are realizable. Cryogenically cooled MOSFETs and MCTs are considered for power conversion and two configurations have been examined. It is found that a system efficiency of 92.67% and specific mass of 9.99 kg/kW/sub e/ can be realized using MOSFET-based cryogenic power conditioning systems for electric propulsion spacecraft using MPD thrusters. With cryogenically cooled MCTs, the specific mass decreases to 9.77 kg/kW/sub e/, but the efficiency also decreases to 90.94%. |
| Starting Page | 605 |
| Ending Page | 610 |
| File Size | 520115 |
| Page Count | 6 |
| File Format | |
| ISBN | 0780335473 |
| ISSN | 10893547 |
| DOI | 10.1109/IECEC.1996.552962 |
| Language | English |
| Publisher | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Publisher Date | 1996-08-11 |
| Publisher Place | USA |
| Access Restriction | Subscribed |
| Rights Holder | Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Subject Keyword | Cryogenics Power conditioning Propulsion Power conversion Mars Process design Electric vehicles Cooling MOSFETs Space vehicles |
| Content Type | Text |
| Resource Type | Article |
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