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Propulsion systems and low-thrust rocket engines based on various physical principles for control systems of small and micro-spacecraft
Ryzhkov V.V., Sulinov A.V.
Mathematical model of turbofan engine weight estimation taking into account the engine configuration and size
Avdeev S.V.
High fidelity modeling at early stages of airframe structural design
Boldyrev A.V., Komarov V.A.
Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines
Kuz'michev V.S., Omar H., Tkachenko A.Y., Bobrik A.A.
Optimal distribution of turboprop engine free energy between the screw and the jet with mass characteristics taken into account
Grigoriev V.A., Prokaev A.S.
Assessing weight efficiency of carrier rockets launched from dirigibles and airplanes
Kurenkov V.I.
Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit
Ishkov S.A.
Influence of the suspension system on the accuracy of the aircraft modal testing results
Berns V.A., Dolgopolov A.V., Zhukov E.P., Marinin D.A.
Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft
Kurenkov V.I., Kucherov A.S., Yakishik A.A.
Assessing reduction gear mass in the problem of optimizing parameters of the working process of a turboprop engine at the initial design stage
Grigoryev V.A., Zagrebelnyi A.O., Prokaev A.S., Kuznetsov S.P.
Methodological support for the training of UAV designers and operators
Lukyanov O.E., Zolotov D.V.
Assessing the efficiency of flights to high near-earth orbits using boosters with chemical and electro-rocket engines
Ishkov S.A., Fadeenkov P.V., Balakin V.L.
1 - 12 of 12 Items

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