THE HYPERSONIC PLASMA CONVERTER: II
Abstract
As a continuation to Part I (SC-4960(RR)) of the hypersonic plasma generator known as ASP (Aerodynamic Supply of Power), experimental analyses have been extended to investigate in detail the various parameters that govern the operation of the generator. A final feasibility study was made, and possible modifications to the theory are outlined. Test runs in the Sandia Corporation arc jet with air as the working fluid at 12,000 BTU/lb have generated 8 amp/sq in short circuit currents and 2.3 volts open circuit voltage. Under favorable conditions, fullsize re-entry vehicles in the altitude range of 200,000 to 80, 000 feet are expected to yield several kilowatts of power.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1964
- Accession Number
- AD0608684
Entities
People
- K. J. Touryan
Organizations
- Lockheed Martin