Accession Number:

AD0701194

Title:

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

Descriptive Note:

Corporate Author:

MCDONNELL DOUGLAS ASTRONAUTICS CO ST LOUIS MO EASTERN DIV

Personal Author(s):

• Bland,M. P.
• Harris ,W. J.

Report Date:

1969-05-09

Pagination or Media Count:

197.0

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