UAH Archives, Special Collections, and Digital Initiatives

"A Practical Approach to the Optimization of the Saturn V Space Vehicle Control System Under Aerodynamic Loads."

Item

Dublin Core

Identifier

spc_stnv_000109

Title

"A Practical Approach to the Optimization of the Saturn V Space Vehicle Control System Under Aerodynamic Loads."

Alternative Title

NASA TM X-53698

Description

This paper includes the equations for the bending moment of a launch vehicle with the effects of bending and sloshing dynamics. It also includes a comparison between the bending moment response envelope of the measure winds and the bending moment response of the MSFC synthetic wind profile.

Date

1965-07-21

Temporal Coverage

Source

Saturn V Collection
Box 14, Folder 30
University of Alabama in Huntsville Archives, Special Collections, and Digital Initiatives, Huntsville, Alabama

Language

Rights

This 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.

Relation

spc_stnv_000075_000118

Is Referenced By

Collection

Citation

Ryan, Robert S. (Robert Samuel), 1925- and Teuber, Dieter, “"A Practical Approach to the Optimization of the Saturn V Space Vehicle Control System Under Aerodynamic Loads.",” UAH Archives, Special Collections, and Digital Initiatives, accessed May 29, 2024, http://libarchstor2.uah.edu/digitalcollections/items/show/2337.

Transcribe This Item

  1. spc_stnv_000109.pdf