Objective of hypersonic propulsion research and design of Hypersonic Propulsion Laboratory at Applied Physics Laboratory of John Hopkins University for inlet and combustion testing of air-breathing engines; program resulted in arc tunnel operation at pressures up to 800 psi, with running times up to 2-min and power inputs (single unit) up to 8.6 Mw; description of h-p arc heaters, power supply, and operating principles and electrode design; performance of arc unit and constructions of Mach 7-10 propulsion tunnel with emphasis on nozzle geometry.
Development of hypersonic propulsion tunnels using D.C. Plasma arc heating
AIAA-ASME -- Paper
AIAA-ASME Hypersonic Ramjet Conference ; 1963 Supersonic
1963
13 pages
Aufsatz (Konferenz)
Englisch
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