Accession Number:

AD0419205

Title:

Development of a High-Temperature Nuclear-Radiation-Resistant Pneumatic Power System for Flight Vehicles

Descriptive Note:

Quarterly rept. 25 June-24 Sep 1963

Corporate Author:

GENERAL DYNAMICS CORP POMONA CA POMONA DIV

Personal Author(s):

Report Date:

1963-09-24

Pagination or Media Count:

38.0

Abstract:

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.

Subject Categories:

  • Research and Experimental Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE