"Saturn IB SA-217 reference launch vehicle."
This document contains a definition of a reference Saturn IB launch vehicle designated SA-217. The Saturn IB SA-217 is a projected reference vehicle, based on Saturn IB SA-212, incorporating the latest proposed product improvements. The two-stage payload capability of this vehicle to a 100-nautical...
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University of Alabama in Huntsville Archives
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Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/10501 |
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Electronic |
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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 "Saturn IB SA-217 reference launch vehicle." Space Vehicle Systems Branch. Propulsion and Vehicle Engineering Laboratory. |
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Documents Saturn project Saturn launch vehicles--Design and construction Saturn 1B launch vehicles |
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This document contains a definition of a reference Saturn IB launch vehicle designated SA-217. The Saturn IB SA-217 is a projected reference vehicle, based on Saturn IB SA-212, incorporating the latest proposed product improvements. The two-stage payload capability of this vehicle to a 100-nautical-mile circular orbit is 44,965 pounds. The Saturn IB SA-217 launch vehicle is to be used as the baseline vehicle for advanced studies requiring the use of the standard or modified Saturn IB launch vehicle. This vehicle definition does not necessarily represent approved changes to any specific vehicle. This document supersedes the Saturn IB SA-213 reference Launch Vehicle, described in memorandum R-P&VE-DIR-65-92. |
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"Saturn IB SA-217 reference launch vehicle."Space Vehicle Systems Branch. Propulsion and Vehicle Engineering Laboratory.Saturn projectSaturn launch vehicles--Design and constructionSaturn 1B launch vehiclesThis document contains a definition of a reference Saturn IB launch vehicle designated SA-217. The Saturn IB SA-217 is a projected reference vehicle, based on Saturn IB SA-212, incorporating the latest proposed product improvements. The two-stage payload capability of this vehicle to a 100-nautical-mile circular orbit is 44,965 pounds. The Saturn IB SA-217 launch vehicle is to be used as the baseline vehicle for advanced studies requiring the use of the standard or modified Saturn IB launch vehicle. This vehicle definition does not necessarily represent approved changes to any specific vehicle. This document supersedes the Saturn IB SA-213 reference Launch Vehicle, described in memorandum R-P&VE-DIR-65-92.1968-01-16TextMemorandumsSaturnIBSA217_052008142122.pdfspc_stnv_000733http://libarchstor2.uah.edu/digitalcollections/items/show/10501http://libarchstor2.uah.edu/digitalcollections/files/original/20/10501/SaturnIBSA217_052008142122.pdfSaturn V CollectionBox 25, Folder 16University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabamaenspc_stnv_000725_000749This 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 |
"Saturn IB SA-217 reference launch vehicle." |
titleStr |
"Saturn IB SA-217 reference launch vehicle." |
author |
Space Vehicle Systems Branch. Propulsion and Vehicle Engineering Laboratory. |
author_facet |
Space Vehicle Systems Branch. Propulsion and Vehicle Engineering Laboratory. |
id |
UAHsaturnv10501 |
url |
http://libarchstor2.uah.edu/digitalcollections/items/show/10501 |
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1790443372876398592 |