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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 |
Analysis of the Main Methods of Obtaining Propellant by Electrolysis of Water
Authors: Shalashov M.A., Peshkov R.A. | Published: 07.03.2022 |
Published in issue: #3(744)/2022 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: oxygen-hydrogen propulsion system, onboard electrolysis unit, small spacecraft |
An Analysis of the Efficiency of Electric Propulsion Engines for Maintaining a Low Orbit of Small Spacecraft
Authors: Volotsuev V.V., Salmin V.V. | Published: 25.09.2020 |
Published in issue: #10(727)/2020 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: small spacecraft, electric propulsion engine, low orbit, orbit correction |