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AIAA R-020A
Recommended Practice for Mass Properties Control for Satellites, Missiles, and Launch Vehicles
| contributor author | AIAA - American Institute of Aeronautics and Astronautics | |
| date accessioned | 2017-09-04T16:01:44Z | |
| date available | 2017-09-04T16:01:44Z | |
| date copyright | 1999.01.01 | |
| date issued | 1999 | |
| identifier other | RLWMPAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsessionid=5419487D58F372296210253C48C0B568/handle/yse/64955 | |
| description abstract | The management and control of mass properties is of fundamental importance in the design and manufacturing process of aerospace hardware. Mass properties are to be managed and controlled as any other system performance parameter. They need to be allocated, analyzed, controlled and verified. The full set of mass properties, including mass, center of gravity, moments of inertia and products of inertia need to be tracked throughout the program to assure compliance with the program requirements. | |
| language | English | |
| title | AIAA R-020A | num |
| title | Recommended Practice for Mass Properties Control for Satellites, Missiles, and Launch Vehicles | en |
| type | standard | |
| page | 19 | |
| status | Active | |
| tree | AIAA - American Institute of Aeronautics and Astronautics:;1999 | |
| contenttype | fulltext |
