Accession Number : AD0701194

Title :   INVESTIGATION OF HIGH ALTITUDE FLIGHT ENVIRONMENTAL EFFECTS ON PURE FLUID AMPLIFIERS AND JET EDGE RESONATOR OSCILLATORS,

Corporate Author : MCDONNELL DOUGLAS ASTRONAUTICS CO ST LOUIS MO EASTERN DIV

Personal Author(s) : Bland,M. P. ; Harris ,W. J.

Report Date : 09 MAY 1969

Pagination or Media Count : 197

Abstract : Four fluid amplifiers, two bistables and two proportionals, were subjected to reduced atmospheric pressures of 14.7, 10, 6, 2, and 0.16 psia. A single jet edge resonator oscillator was tested at the above pressures at each of the following temperatures: 72, 210, 350, and 500F. The report describes the results of these tests. (Author)

Descriptors :   (*FLUID AMPLIFIERS, AEROSPACE CRAFT), (*OSCILLATORS, *FLUIDICS), HIGH ALTITUDE, ENVIRONMENTAL TESTS, RESONATORS, CONTROL SYSTEMS

Subject Categories : Research and Experimental Aircraft
      Fluidics and Fluerics
      Unmanned Spacecraft

Distribution Statement : APPROVED FOR PUBLIC RELEASE