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Apollo Soyuz Test Project Weights and Mass Properties Operational Management SystemThe Apollo Soyuz Test Project (ASTP) Weights and Mass Properties Operational Management System was established to assure a timely and authoritative method of acquiring, controlling, generating, and disseminating an official set of vehicle weights and mass properties data. This paper provides an overview of the system and its interaction with the various aspects of vehicle and component design, mission planning, hardware and software simulations and verification, and real-time mission support activities. The effect of vehicle configuration, design maturity, and consumables updates is discussed in the context of weight control.
Document ID
19750063415
Document Type
Conference Paper
Authors
Collins, M. A., Jr.
Hischke, E. R. (NASA Johnson Space Center Houston, Tex., United States)
Date Acquired
August 8, 2013
Publication Date
May 1, 1975
Subject Category
SPACECRAFT DESIGN, TESTING AND PERFORMANCE
Report/Patent Number
SAWE PAPER 1049
Meeting Information
Society of Allied Weight Engineers, Annual Conference(Seattle, WA)
Distribution Limits
Public
Copyright
Other