"A 'Zero Stage' for the Saturn IB Launch Vehicle."
To meet the demands of increasing payload size and weight, and to fill the large payload gap between the Saturn IB and Saturn V, a number of methods of uprating the Saturn IB have been studied by NASA and Chrysler Corp. of providing increased payload capability is discussed in this paper. Four 120...
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University of Alabama in Huntsville Archives
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Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/10244 |
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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 "A 'Zero Stage' for the Saturn IB Launch Vehicle." Vehko, Vaino J. |
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Documents Saturn project Saturn launch vehicles Solid propellant rockets Saturn 1B launch vehicles Spacecraft propulsion |
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To meet the demands of increasing payload size and weight, and to fill the large payload gap between the Saturn IB and Saturn V, a number of methods of uprating the Saturn IB have been studied by NASA and Chrysler Corp. of providing increased payload capability is discussed in this paper. Four 120 in. United Technology Center UA-1205 solid propellant motors, originally developed for the Air Force Titan III program, are clustered around the S-IB first stage of the Saturn IB launch vehicle. These four solid propellant motors provide the total thrust for liftoff of the vehicle, with S-IB stage ignition occurring just prior to burn-out and separation of the solid propellant motors. The term "Zero Stage" is applied to this added stage. |
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"A 'Zero Stage' for the Saturn IB Launch Vehicle."Vehko, Vaino J.Ruhland, William E.Saturn projectSaturn launch vehiclesSolid propellant rocketsSaturn 1B launch vehiclesSpacecraft propulsionTo meet the demands of increasing payload size and weight, and to fill the large payload gap between the Saturn IB and Saturn V, a number of methods of uprating the Saturn IB have been studied by NASA and Chrysler Corp. of providing increased payload capability is discussed in this paper. Four 120 in. United Technology Center UA-1205 solid propellant motors, originally developed for the Air Force Titan III program, are clustered around the S-IB first stage of the Saturn IB launch vehicle. These four solid propellant motors provide the total thrust for liftoff of the vehicle, with S-IB stage ignition occurring just prior to burn-out and separation of the solid propellant motors. The term "Zero Stage" is applied to this added stage.3/1/1966TextReportszerostage_082707085507.pdfspc_stnv_000942http://libarchstor2.uah.edu/digitalcollections/items/show/10244http://libarchstor2.uah.edu/digitalcollections/files/original/20/10244/zerostage_082707085507.pdfSaturn V CollectionBox 16, Folder 23University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabamaenspc_stnv_000925_000942This 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 |
"A 'Zero Stage' for the Saturn IB Launch Vehicle." |
titleStr |
"A 'Zero Stage' for the Saturn IB Launch Vehicle." |
author |
Vehko, Vaino J. |
author_facet |
Vehko, Vaino J. Ruhland, William E. |
author2 |
Ruhland, William E. |
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UAHsaturnv10244 |
url |
http://libarchstor2.uah.edu/digitalcollections/items/show/10244 |
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1790443372618448896 |