DocumentCode
1176846
Title
Alternate Mode of Operation Program
Author
Paris, T.W., Jr.
Author_Institution
General Electric Company Apollo Support Department Cape Canaveral, Florida
Issue
4
fYear
1966
fDate
7/1/1966 12:00:00 AM
Firstpage
771
Lastpage
776
Abstract
The increasing complexity of the launch support equipment and the narrow launch windows of the Saturn IB and Saturn V missions require that methods be developed to minimize any delay attributable to launch support equipment failures. Since even short delays cannot be tolerated for Saturn manned missions, it is necessary to develop a method to prevent the occurrence of these delays. The Alternate Mode of Operation (AMO) concept, an analytical methodology, can be used to achieve this goal. The AMO Program is an engineering analysis of launch support equipment consisting of three phases. a. The design analysis phase which consists of performing the analysis as soon as the preliminary design is completed and constructing failure isolation logic diagrams. b. The operations analysis phase which consists of validating the failure isolation procedures, making launch decisions prior to the countdown which may result in built-in holds, and establishing repair plans prior to the countdown for personnel familiarization. c. The implementation phase which consists of instantly displaying the failure isolation logic and launch decisions for use by personnel in case of equipment failure during the countdown. The Alternate Mode of Operation Program provides: a. Launch support equipment capable of meeting launch windows. b. Optimized failure isolation procedures. c. Predetermined launch decisions in case of launch support equipment failure during the countdown.
Keywords
Apertures; Control systems; Delay; Displays; Equipment failure; Failure analysis; Logic design; Performance analysis; Personnel; Saturn;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.1966.4501911
Filename
4501911
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