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Concept Verification Test - Evaluation of Spacelab/Payload operation conceptsThe Concept Verification Test (CVT) procedure is used to study Spacelab operational concepts by conducting mission simulations in a General Purpose Laboratory (GPL) which represents a possible design of Spacelab. In conjunction with the laboratory a Mission Development Simulator, a Data Management System Simulator, a Spacelab Simulator, and Shuttle Interface Simulator have been designed. (The Spacelab Simulator is more functionally and physically representative of the Spacelab than the GPL.) Four simulations of Spacelab mission experimentation were performed, two involving several scientific disciplines, one involving life sciences, and the last involving material sciences. The purpose of the CVT project is to support the pre-design and development of payload carriers and payloads, and to coordinate hardware, software, and operational concepts of different developers and users.
Document ID
19770053700
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Mcbrayer, R. O.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Watters, H. H.
(NASA Marshall Space Flight Center Man/Systems Integration Branch, Huntsville, Ala., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AAS 75-239
Meeting Information
Meeting: Annual Meeting on Space shuttle missions of the 80''s
Location: Denver, CO
Start Date: August 26, 1975
End Date: August 28, 1975
Accession Number
77A36552
Distribution Limits
Public
Copyright
Other

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