Increasing the efficiency of combined control of the rocket engine thrust vector
This paper focuses on the drawback of the new concept of thrust vector control, which consists in the need for heavy-mass drives to rotate engine components. The paper presents and substantiates a new solution on eliminating the above drawback by transferring the function of the rotary drives to the...
Збережено в:
| Дата: | 2019 |
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| Автори: | , , |
| Формат: | Стаття |
| Мова: | English |
| Опубліковано: |
Інститут технічної механіки НАН України і НКА України
2019
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| Назва видання: | Технічна механіка |
| Онлайн доступ: | http://dspace.nbuv.gov.ua/handle/123456789/174037 |
| Теги: |
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| Назва журналу: | Digital Library of Periodicals of National Academy of Sciences of Ukraine |
| Цитувати: | Increasing the efficiency of combined control of the rocket engine thrust vector / N.S. Pryadko, N.P. Syrotkina, E.L. Tokareva // Технічна механіка. — 2019. — № 2. — С. 30-38. — Бібліогр.: 12 назв. — англ. |
Репозитарії
Digital Library of Periodicals of National Academy of Sciences of Ukraine| Резюме: | This paper focuses on the drawback of the new concept of thrust vector control, which consists in the need for heavy-mass drives to rotate engine components. The paper presents and substantiates a new solution on eliminating the above drawback by transferring the function of the rotary drives to the gas-dynamic system. |
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