Published January 20, 1993 | Version v1
Journal article

Pulsed inductive thruster performance data base for megawatt-class engine applications

  • 1. TRW Space and Technology Group, One Pace Park, Redondo Beach, CA 90278 (United States)
  • 2. University of California at San Diego, 4744 Panorama Drive, San Diego, CA 92116 (United States)

Description

The pulsed inductive thruster (PIT) is an electrodeless plasma accelerator employing a large (1m diameter) spiral coil energized by a capacitor bank discharge. The bank can be repetitively recharged by a nuclear electric generator for continuous MW level operation. The coil can be designed as a transformer that permits thruster operation at the generator voltage, which results in a low thruster specific mass. Specific impulse (Isp) can be readily altered by changing the propellant valve plenum pressure. Performance curves generated from mesausred impulse, injected mass and capacitor bank energy are presented for argon, ammonia, hydrazine, carbon dioxide and helium. The highest performance measured to date is 48% efficiency at 4000 seconds Isp with ammonia. The development of a theoretical model of the thruster, which assumes a fully ionized plasma, is presented in an appendix

Additional details

Publishing Information

Journal Title
AIP Conference Proceedings
Journal Volume
271
Journal Issue
3
Journal Page Range
p. 1425-1434.
ISSN
0094-243X
CODEN
APCPCS

Conference

Title
10. symposium on space nuclear power and propulsion.
Dates
10-14 Jan 1993.
Place
Albuquerque, NM (United States).

Optional Information

Secondary number(s)
CONF-930103--.