Status review of liquid rocket static test range at Iowa State UniversityThe 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.
Document ID
19760063126
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brodsky, R. F. (Iowa State University of Science and Technology, Ames, Iowa, United States)