UAH Archives, Special Collections, and Digital Initiatives

"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

Type

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 July 23, 2024, http://libarchstor2.uah.edu/digitalcollections/items/show/11154.

Transcribe This Item

  1. Deciprocforminicost_100107112756.pdf