The 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.
Apollo Soyuz Test Project Weights and Mass Properties Operational Management System
Society of Allied Weight Engineers, Annual Conference ; 1975 ; Seattle, WA
1975-05-01
Conference paper
No indication
English
NTIS | 1975
NTRS | 1975
NTIS | 1975
NTRS | 1974
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