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All articles by "Kirievskii D.A."
Approximate determination of losses in characteristic velocity and increments in flight altitude of the multistage launch vehicle upper stages
| Authors: Mukhamedov L.P., Kirievskii D.A. | Published: 13.08.2023 |
| Published in issue: #8(761)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: losses in characteristic velocity, design-ballistic problems, design-ballistic parameters, launch vehicle |
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 |
Approximate Methodology for Design Ballistic Calculation of Two-Stage Launch Vehicles
| Authors: Mukhamedov L.P., Kirievskii D.A. | Published: 27.01.2022 |
| Published in issue: #2(743)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: design ballistic calculation method, design ballistics problems, design ballistic parameters, launch vehicle, characteristic velocity losses |
Approximate Methodology for Design Ballistic Calculations of the First Stage of Launch Vehicles
| Authors: Mukhamedov L.P., Kirievskii D.A. | Published: 27.06.2020 |
| Published in issue: #6(723)/2020 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: design ballistic calculation methods, design ballistics tasks, design and ballistic parameters, launch vehicle, launch vehicle flight characteristics, characteristic speed losses |