MIL-STD-176A
FOREWORD
This revision to MIL-STD-176 dated 1 March 1955 is based on the
cooperative efforts of the Military Services, Weight Engineers of the
Missile Industry, representatives of the National Aeronautics and Space
Administration, the National Committee of the Society of Aeronautical
Weight Engineers and the Aero Space Industries Association.
In general, this standard provides for the mass properties reporting
of the complete spectrum of small and large missiles and space launch
vehicles. These reported data provide the technical background for weight
control engineering, weight optimization studies, the derivation of pro-
posal analysis techniques and provides inputs to industrial planning re-
ports for measuring the national industrial effort.
The standard follows the general philosophy used in MIL-STD-254
Weight and Balance Data Reporting Forms for Aircraft and MIL-STD-
451 Weight and Balance Report Forms for Rotocraft and is adaptable to
either manual or machine method preparation.
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