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The Influence of Configuration on the Range of a Hypersonic Flight Vehicle under Space Limitations
| Authors: Presnyakov S.V., Usachev V.A., Koryanov V.V., Kudryavtseva N.V. | Published: 16.12.2019 |
| Published in issue: #12(717)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: ram jet, solid propellant engine, combustion chamber pressure, configuration, mass efficiency, maximum range |
