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Status review of liquid rocket static test range at Iowa State University

Authors :
Brodsky, R. F
Publication Year :
1976
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1976.

Abstract

The liquid rocket static test range of the Iowa State University incorporates an Aerobee sustainer propulsion system consisting of a pressure fed (helium) liquid bipropellant (hypergolic) rocket engine with a regeneratively fuel-cooled thrust chamber assembly. The paper covers test results to date (including results of four test firings in the water expulsion mode), construction details of the test stand, the laboratory course syllabus, and the environmental impact statement.

Details

Language :
English
Database :
NASA Technical Reports
Publication Type :
Report
Accession number :
edsnas.19760063126
Document Type :
Report