Selecting optimum design of Cyclone-4 stage 1 propellant tank intake
The residues of rocket propellant in tanks after the launch vehicle stage burnout have a substantial influence on the launch vehicle power budget. In modern launch vehicle tanks, the intakes maintain the continuous supply of propellants from a tank to the propulsion system, keeping the continuity of...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
National Aerospace University «Kharkiv Aviation Institute»
2022-02-01
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| Series: | Авіаційно-космічна техніка та технологія |
| Subjects: | |
| Online Access: | http://nti.khai.edu/ojs/index.php/aktt/article/view/1642 |