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Selection of the optimal thrust-to-weight ratio of the first stages of small-lift launch vehicles
| Authors: Mukhamedov L.P., Kirievskii D.A. | Published: 04.06.2023 |
| Published in issue: #6(759)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: ballistic design problem, ballistic design parameters, ultralight launch vehicle, small spacecraft, characteristic velocity losses |
