Application of redundancy in the Saturn V guidance and control system.Application of redundancy in Saturn V guidance and control system to achieve desired reliability
Document ID
19670057221
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Moore, F. B.
White, J. B.
Date Acquired
August 3, 2013
Publication Date
August 1, 1967
Subject Category
Navigation
Report/Patent Number
AIAA PAPER 67-553
Accession Number
67A35950
Distribution Limits
Public
Copyright
Other
Keywords
SATURN V LAUNCH VEHICLEREDUNDANT SYSTEMSPACECRAFT RELIABILITYGUIDANCE AND CONTROL