"Decision Procedure for Minimizing Costs of Calibrating Liquid Rocket Engines."
Item
Dublin Core
Identifier
Deciprocforminicost_100107112756.pdf
spc_stnv_000227
Title
"Decision Procedure for Minimizing Costs of Calibrating Liquid Rocket Engines."
Description
Prior to acceptance of a liquid rocket engine for use in Saturn vehicles, the average thrust of two consecutive tests without an intervening calibration must satisfy specification requirements. The contractor may recalibrate after the first and subsequent tests if he so chooses, based upon decision limits, until the above requirement is met.
Date
1965-10-01
Temporal Coverage
Source
Saturn V Collection
Box 15, Folder 9
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_000225_000249
Is Referenced By
<a href="http://libarchstor.uah.edu:8081/repositories/2/archival_objects/17340"> View this item in ArchivesSpace </a>
Collection
Citation
Lishman, Sidney H. and Bombara, E. L., “"Decision Procedure for Minimizing Costs of Calibrating Liquid Rocket Engines.",” UAH Archives, Special Collections, and Digital Initiatives, accessed November 9, 2024, http://libarchstor2.uah.edu/digitalcollections/items/show/11154.