NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
High energy density capacitors for vacuum operation with a pulsed plasma loadResults of the effort of designing, fabricating, and testing of a 40 joules/lb (88.2 joules/Kg) high voltage energy storage capacitor suitable for operating a pulsed plasma thruster in a vacuum environment for millions of pulses are presented. Using vacuum brazing and heli-arc welding techniques followed by vacuum and high pressure helium leak tests it was possible to produce a hermetically sealed relatively light weight enclosure for the dielectric system. An energy density of 40 joules/lb was realized with a KF-polyvinylidene fluoride dielectric system. One capacitor was D.C. life tested at 4 KV (107.8 joules/lb) for 2,000 hours before it failed. Another exceeded 2,670 hours without failure at 38.3 joules/lb. Pulse life testing in a vacuum exceeded 300,000 discharges with testing still in progress. The D.C. life test data shows a small decrease in capacitance and an increase in dissipation factor with time. Heat transfer from the load to the capacitor must also be considered besides the self-heat generated by the capacitor.
Document ID
19770012222
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Guman, W. J.
(Fairchild Republic Co. Farmingdale, NY, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1976
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-149813
Report Number: NASA-CR-149813
Accession Number
77N19166
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: JPL-953656
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available