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Experimental investigation of the pulsed electrothermal (PET) thrusterBurton et al. (1982) have discussed the theory of the Pulsed Electrothermal (PET) thruster, a device which in principle can operate with 70 percent efficiency at a specific impulse of 1000 seconds and higher. It is pointed out that this level of performance would be particularly attractive for orbit raising of large satellites and other near-earth missions, which cannot be easily accomplished by chemical propulsion. The present investigation is concerned with two PET thruster operating modes. A PET thruster was built and tested on a thrust stand. Exhaust velocities for polyethylene propellant vary from 20 to 27 km/sec. Single pulse specific impulse and efficiency measurements based on ablated mass show a thruster efficiency of 37-56 percent in the time range from 1000 to 1750 seconds. It is believed that an improved design with a thruster efficiency in the range from 70 to 80 percent might be possible.
Document ID
19840052414
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Burton, R. L.
(GT-Devices Alexandria, VA, United States)
Goldstein, S. A.
(GT-Devices Alexandria, VA, United States)
Hiko, B. K.
(GT-Devices Alexandria, VA, United States)
Tidman, D. A.
(GT-Devices Alexandria, VA, United States)
Winsor, N. K.
(GT-Devices, Inc. Alexandria, VA, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1984
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 84-1386
Accession Number
84A35201
Funding Number(s)
CONTRACT_GRANT: NAS3-23866
CONTRACT_GRANT: NAS3-23779
Distribution Limits
Public
Copyright
Other

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