AIAA R 020 : A1999
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
RECOMMENDED PRACTICE FOR MASS PROPERTIES CONTROL FOR SATELLITES, MISSILES, AND LAUNCH VEHICLES
Published date
12-01-2013
Withdrawn date
23-07-2013
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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.
| DocumentType |
Standard
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| PublisherName |
American Institute of Aeronautics & Astronautics
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| Status |
Withdrawn
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| BS ISO 22010:2007 | Space systems. Mass properties control |
| AIAA R 021 : 1992 | RECOMMENDED PRACTICE FOR SPACECRAFT SYSTEM DESIGN IN SI UNITS |
| AIAA G 020 : 1992 | GUIDE FOR ESTIMATING AND BUDGETING WEIGHT AND POWER CONTINGENCIES FOR SPACECRAFT SYSTEMS |
| ISO 22010:2007 | Space systems — Mass properties control |
| AIAA R 060 : 1993 | RECOMMENDED PRACTICE FOR REPORTING EARTH-TO-ORBIT MISSION PROFILES |
| AIAA G 056 : 1992 | Guide: Guide to the Serviceable Spacecraft Grasping/Berthing/Docking Interfaces |
| AIAA R 060 : 1993 | RECOMMENDED PRACTICE FOR REPORTING EARTH-TO-ORBIT MISSION PROFILES |
| AIAA G 020 : 1992 | GUIDE FOR ESTIMATING AND BUDGETING WEIGHT AND POWER CONTINGENCIES FOR SPACECRAFT SYSTEMS |
| AIAA G 056 : 1992 | Guide: Guide to the Serviceable Spacecraft Grasping/Berthing/Docking Interfaces |
| AIAA R 021 : 1992 | RECOMMENDED PRACTICE FOR SPACECRAFT SYSTEM DESIGN IN SI UNITS |
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