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Parametric analysis of hollow conductor parallel and coaxial transmission lines for high frequency space power distributionA parametric analysis was performed of transmission cables for transmitting electrical power at high voltage (up to 1000 V) and high frequency (10 to 30 kHz) for high power (100 kW or more) space missions. Large diameter (5 to 30 mm) hollow conductors were considered in closely spaced coaxial configurations and in parallel lines. Formulas were derived to calculate inductance and resistance for these conductors. Curves of cable conductance, mass, inductance, capacitance, resistance, power loss, and temperature were plotted for various conductor diameters, conductor thickness, and alternating current frequencies. An example 5 mm diameter coaxial cable with 0.5 mm conductor thickness was calculated to transmit 100 kW at 1000 Vac, 50 m with a power loss of 1900 W, an inductance of 1.45 micron and a capacitance of 0.07 micron-F. The computer programs written for this analysis are listed in the appendix.
Document ID
19840012571
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jeffries, K. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Renz, D. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1984
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-2013
NAS 1.15:83601
NASA-TM-83601
Report Number: E-2013
Report Number: NAS 1.15:83601
Report Number: NASA-TM-83601
Accession Number
84N20639
Funding Number(s)
PROJECT: RTOP 506-55-72
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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