AIAA R 021 : 1992
Withdrawn
Withdrawn
RECOMMENDED PRACTICE FOR SPACECRAFT SYSTEM DESIGN IN SI UNITS
Published date
01-12-2013
Withdrawn date
07-23-2013
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Gives method to simplify the transfer from conventional (U.S.) notation systems to the International System (SI) of units. Recommends that new items, equipment, or systems be designed in metric units, rather than converting existing designs. References several other documents to provide the basis for SI application to spacecraft system design practice. Intended for use in hardware design and development, as well as research and all published documents.
| DocumentType |
Standard
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| PublisherName |
American Institute of Aeronautics & Astronautics
|
| Status |
Withdrawn
|
| AIAA G 020 : 1992 | GUIDE FOR ESTIMATING AND BUDGETING WEIGHT AND POWER CONTINGENCIES FOR SPACECRAFT SYSTEMS |
| AIAA R 020 : A1999 | RECOMMENDED PRACTICE FOR MASS PROPERTIES CONTROL FOR SATELLITES, MISSILES, AND LAUNCH VEHICLES |
| AIAA G 056 : 1992 | Guide: Guide to the Serviceable Spacecraft Grasping/Berthing/Docking Interfaces |
| AIAA R 020 : A1999 | RECOMMENDED PRACTICE FOR MASS PROPERTIES CONTROL FOR SATELLITES, MISSILES, AND LAUNCH VEHICLES |
| 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 |
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