AIAA R 020 : A1999
Current
The latest, up-to-date edition.
RECOMMENDED PRACTICE FOR MASS PROPERTIES CONTROL FOR SATELLITES, MISSILES, AND LAUNCH VEHICLES
01-12-2013
Gives a comprehensive methodology for mass properties control through the multiple phases of space hardware development. It defines the development stages, describes a control process which meets expectations in all sectors of the aerospace industry, and establishes analytical and verification techniques which assure operation within established limits.
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