AIAA R 020 : A1999
Current
The latest, up-to-date edition.
RECOMMENDED PRACTICE FOR MASS PROPERTIES CONTROL FOR SATELLITES, MISSILES, AND LAUNCH VEHICLES
12-01-2013
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.
| DocumentType |
Standard
|
| PublisherName |
American Institute of Aeronautics & Astronautics
|
| Status |
Current
|
| 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<br> |
| 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<br> |
| AIAA R 021 : 1992 | RECOMMENDED PRACTICE FOR SPACECRAFT SYSTEM DESIGN IN SI UNITS |
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