CALCULATION OF THE OPTIMAL DIAMETER OF THE AIR INTAKE OF THE PROPULSION SYSTEM FOR SMALL SPACECRAFT
Background. In connection with the increasing interest in the Russian Federation in programs for the development of near-Earth spacecraft, studies have been carried out on the optimal diameter of the grid channel of the air intake of the propulsion system of a small spacecraft operating on outboar...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Penza State University Publishing House
2022-10-01
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| Series: | Надежность и качество сложных систем |
| Subjects: |