Author: Andre LeBlancPublisher:
ISBN:
Category : Plasma (Ionized gases)
Languages : en
Pages : 438
Book Description
Hypersonic Plasma Thermionic Generator
Author: Andre LeBlancPublisher:
ISBN:
Category : Plasma (Ionized gases)
Languages : en
Pages : 438
Book Description
The Hypersonic Plasma Converter: I
Author: K. J. TouryanPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 42
Book Description
Theoretical and experimental analyses are presented which describe the operation of the hypersonic plasma generator as ASP (Aerodynamic Supply of Power). Previous investigations are reviewed, corrected and summarized. Additional information is introduced to bring the present status of the generator up to date.
Hypersonic Plasma Thermionic Generator
Author: William J. ByattPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 38
Book Description
Hypersonic Plasma Thermionic Generator
Author: Andre LeBlancPublisher:
ISBN:
Category : Plasma generators
Languages : en
Pages : 228
Book Description
Hypersonic Plasma Thermionic Generator
Author: Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 38
Book Description
Hypersonic Plasma Thermionic Generator
Author: C. W. BryanPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 28
Book Description
Special Materials Tests for the Hypersonic Plasma Generator
Author: K. J. TouryanPublisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 16
Book Description
The Hypersonic Plasma Converter: II
Author: K. J. TouryanPublisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 50
Book Description
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. (Author).
Author: 
Author: