Altitude Simulation in Saturn S-IV Stage Testing

640282

01/01/1964

Event
SAE World Congress & Exhibition
Authors Abstract
Content
The Douglas Aircraft Co. has been involved in testing the Saturn S-IV stage at the Sacramento Test Center for the past two years. The propulsion system for the S-IV stage consists of six Pratt & Whitney Aircraft Co. rocket engines specifically designed for high-altitude start and operation. During static firing tests of this engine at sea level, a steam jet ejector in combination with a diffuser is used to simulate altitude conditions. The intent of this paper is to examine the performance of this altitude simulation system, and to discuss the problems encountered in making it operational.
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DOI
https://doi.org/10.4271/640282
Pages
8
Citation
Hofferth, D., Wilson, E., and Polansky, A., "Altitude Simulation in Saturn S-IV Stage Testing," SAE Technical Paper 640282, 1964, https://doi.org/10.4271/640282.
Additional Details
Publisher
Published
Jan 1, 1964
Product Code
640282
Content Type
Technical Paper
Language
English