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Methodological principles of space vehicle design for the maximum energy sup-ply of the payload
Chebotarev V., Fatkulin R., Vorontsova E., Balandina T., Shangina E.
The concept of an educational and scientific experiment for conducting on-orbit testing of any types of photovoltaic cell
Lukyanov M., Prokhorov G., Kutsenko V., Parshin A., Zuev D.
Methodological principles for the formation of a number of unified space communication satellite platforms
Chebotarev V., Zimin I., Vnukov A., Shangina E.
Development of the CYCLOPS CubeSat payload
Sotnikova N., Kadadova A., Utkin V., Kadochnikov D.
STATISTICAL ANALYSIS OF THE RELATIONSHIP OF CONSTRUCTIVE CHARACTERISTICS OF AIRCRAFTS
Balaban E., Bunakov P., Gal’chenko A., Tegin V.
Design of a thermal control system with a two-phase coolant for a spacecraft with a capacity of 7 kW
Shilkin O., Kolesnikov A., Delkov A., Kishkin A., Shevchenko Y.
Тhe analysis of dependence of durability, risk of accidents and efficiency of transportations on airplane construction weight
Boyko O.
METHODOLOGICAL BASES OF ESTIMATION OF SYSTEMIC ACTION OF ADDITIONAL PAYLOAD ON SPACECRAFT FUNCTIONING
Kislitskiy M.
THE DEPENDENCE ANALYSIS OF DURABILITY, THE CATASTROPHE RISK AND THE TRANSPORT EFFECTIVENESS ON THE AIRPLANE CONSTRUCTION MASS
Boyko O.
THE CHOICE OF HEAT-ACCUMULATING MATERIALS FOR SOLAR THERMAL PROPULSION
Finogenov S., Kolomentsev A.
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