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The problem of ensuring and controlling microaccelerations in the internal environment of a small technological spacecraft |
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| รหัสดีโอไอ | |
| Creator | A. S. Taneeva |
| Title | The problem of ensuring and controlling microaccelerations in the internal environment of a small technological spacecraft |
| Contributor | A. V. Sedelnikov, E. V. Eskina, E. S. Khnyryova, and M. E. Bratkova |
| Publisher | Rangsit University |
| Publication Year | 2566 |
| Journal Title | ๋Journal of Current Science and Technology |
| Journal Vol. | 13 |
| Journal No. | 1 |
| Page no. | 1-11 |
| Keyword | gravity-sensitive process, internal environment, microacceleration, operating principles, small spacecraft |
| URL Website | https://jcst.rsu.ac.th |
| ISSN | 2630-0656 |
| Abstract | This paper gives reviews approaches to reduce microaccelerations in the internal environment of a small spacecraft and provides quantitative estimation of the level of microaccelerations. These approaches involve the reduction of microaccelerations in the entire internal environment of the spacecraft or the creation of a protected zone using vibration-isolating devices. In the latter case, gravity-sensitive processes can be performed only inside this zone. Various vibration-isolating devices based on various operating principles are considered. These anti-vibration devices have been experimentally tested under space flight conditions on various spacecraft. In this study, they are considered as ready-made solutions for the creation of a small technological spacecraft. A small technological spacecraft design was developed, and the issues of ensuring the quality of the obtained results of gravity-sensitive processes by controlling the level of microaccelerations were considered. The results can be used in the design and operation of small technological spacecraft. |
