AIAA G 020 : 1992
Withdrawn
Withdrawn
GUIDE FOR ESTIMATING AND BUDGETING WEIGHT AND POWER CONTINGENCIES FOR SPACECRAFT SYSTEMS
Published date
01-12-2013
Withdrawn date
07-23-2013
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Provides minimum weight and electrical power contingency requirements for the development and design of all spacecraft, systems, subsystems, components, and parts. It provides a detailed description of the stages of development and classes of design maturity. Contains provisions for the control of design parameters during each stage for each of four categories of weight or power.
| DocumentType |
Standard
|
| PublisherName |
American Institute of Aeronautics & Astronautics
|
| Status |
Withdrawn
|
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Sorry this product is not available in your region.