Methodology of designing a small spacecraft for technological purposes
The paper presents a methodology for designing a small spacecraft to perform the tasks of technological processes in near-Earth space. When designing such a small spacecraft, it is assumed that it will be equipped with a microgravity platform to meet the requirements for micro-accelerations. The...
Saved in:
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Omsk State Technical University, Federal State Autonomous Educational Institution of Higher Education
2024-12-01
|
| Series: | Омский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение" |
| Subjects: | |
| Online Access: | https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2024/%D0%A2.8,%20%E2%84%964%20(%D0%90%D0%A0%D0%B8%D0%AD%D0%9C)/73-79%20%D0%A1%D0%B5%D0%B4%D0%B5%D0%BB%D1%8C%D0%BD%D0%B8%D0%BA%D0%BE%D0%B2%20%D0%90.%20%D0%92.,%20%D0%A2%D0%B0%D0%BD%D0%B5%D0%B5%D0%B2%D0%B0%20%D0%90.%20%D0%A1..pdf |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| Summary: | The paper presents a methodology for designing a small spacecraft to perform the tasks of
technological processes in near-Earth space. When designing such a small spacecraft, it is assumed that
it will be equipped with a microgravity platform to meet the requirements for micro-accelerations.
The methodology is based on the principles of individuality, attainability and controllability. They
guarantee the maximum possible consideration of the features of the gravity-sensitive process
being implemented, including compliance with the requirements for limiting the micro-acceleration
module in the working area of technological equipment and effective control of this implementation.
The developed technique can be used in the design of a small spacecraft for technological purposes. |
|---|---|
| ISSN: | 2588-0373 2587-764X |