Accession Number:

AD0872090

Title:

Development of a Three-Stage Supersonic Hot Gas Reaction Valve,

Personal Author(s):

Corporate Author:

ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL GUI DANCE AND CONTROL DIRECTORATE

Report Date:

1968-09-17

Abstract:

The purpose of the report is to describe briefly the performance of a three-stage, fluidic, hot gas, jet reaction control valve developed for the MARS flight control system. Author

Pages:

0087

Descriptors:

Identifiers:

Subject Categories:

File Size:

0.00MB

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