"Altitude Simulation in Saturn SIV Space Testing."
This paper was presented to the Society of Automotive Engineers. The abstract reads, "The Douglas Aircraft Company has been involved in testing the Saturn SIV stage at the Sacramento Test Center for the past two years. The propulsion system for the SIV stage consists of six (6) Pratt & Wh...
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University of Alabama in Huntsville Archives
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Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/1143 |
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Saturn V Collection |
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University of Alabama in Huntsville Archives |
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University of Alabama in Huntsville Archives |
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Documents "Altitude Simulation in Saturn SIV Space Testing." Hofferth, D. D. |
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Documents Saturn Project (U.S.) Saturn launch vehicles--Testing Saturn S-4 stage Altitude simulation |
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This paper was presented to the Society of Automotive Engineers. The abstract reads, "The Douglas Aircraft Company has been involved in testing the Saturn SIV stage at the Sacramento Test Center for the past two years. The propulsion system for the SIV stage consists of six (6) Pratt & Whitney Aircraft Company rocket engines which are designed specifically 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, are used to simulate altitude conditions. The intent of this paper is to examine the performance of this altitude simulation system, and to discuss problems encountered in making it operational." |
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"Altitude Simulation in Saturn SIV Space Testing."Hofferth, D. D.Polansky, A. L.Wilson, E. L.Douglas Aircraft Company. Missile and Space Systems DivisionSaturn Project (U.S.)Saturn launch vehicles--TestingSaturn S-4 stageAltitude simulationThis paper was presented to the Society of Automotive Engineers. The abstract reads, "The Douglas Aircraft Company has been involved in testing the Saturn SIV stage at the Sacramento Test Center for the past two years. The propulsion system for the SIV stage consists of six (6) Pratt & Whitney Aircraft Company rocket engines which are designed specifically 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, are used to simulate altitude conditions. The intent of this paper is to examine the performance of this altitude simulation system, and to discuss problems encountered in making it operational."1965-01-01ReportsTextspc_stnv_000059http://libarchstor2.uah.edu/digitalcollections/items/show/1143http://libarchstor2.uah.edu/digitalcollections/files/original/20/1143/spc_stnv_000059.pdfSaturn V CollectionBox 12, Folder 60University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabamaenspc_stnv_000051_000074This material may be protected under U. S. Copyright Law (Title 17, U.S. Code) which governs the making of photocopies or reproductions of copyrighted materials. You may use the digitized material for private study, scholarship, or research. Though the University of Alabama in Huntsville Archives and Special Collections has physical ownership of the material in its collections, in some cases we may not own the copyright to the material. It is the patron's obligation to determine and satisfy copyright restrictions when publishing or otherwise distributing materials found in our collections. |
title |
"Altitude Simulation in Saturn SIV Space Testing." |
titleStr |
"Altitude Simulation in Saturn SIV Space Testing." |
author |
Hofferth, D. D. |
author_facet |
Hofferth, D. D. Polansky, A. L. Wilson, E. L. Douglas Aircraft Company. Missile and Space Systems Division |
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Polansky, A. L. Wilson, E. L. Douglas Aircraft Company. Missile and Space Systems Division |
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UAHsaturnv1143 |
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http://libarchstor2.uah.edu/digitalcollections/items/show/1143 |
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1790443371696750592 |