Development of a High-Temperature Nuclear-Radiation-Resistant Pneumatic Power System for Flight Vehicles
Quarterly rept. 25 June-24 Sep 1963
GENERAL DYNAMICS CORP POMONA CA POMONA DIV
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The preliminary study for Phase II of the turbo compressor program was completed a satisfactory configuration was established for a four-stage centrifugal compressor utilizing a single shaft. Three high-temperature 1,500 deg F experimental test runs were conducted on the pilot portion of the Model X pressure regulator while experimental room temperature testing of the Model F relief valves also was completed with satisfactory results.
- Research and Experimental Aircraft