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Authors
The problems of creating a propulsion system of a new generation supersonic passenger aircraft (review)
Alendar A.D., Lanshin A.I., Evstigneev A.A., Yakubovsky K.Y., Siluyanova M.V.
Assessment of the possibility of shortening the landing distance of maneuverable aircraft
Strelets M.Y., Tarasov A.Z., Grishin I.A.
Methodology for thermal calculation of the heat exchanger for cooling the air at the intake of the aerospace plane engine compressor
Panchenko S.L., Gras’ko T.V.
Method of first-approximation calculation of take-off weight of a light aircraft with a hybrid propulsion system
Sychev A.V., Arbuzov I.V., Ravikovich Y.A.
Aircraft electric power plants
Kondryakov A.D., Leontiev M.K.
Power plants of the first aircraft
Drygin A.S.
Survey of the flight efficiency of a long-haul aircraft under uncertainty of tasks
Markiewicz P.
Investigations for landing gear rational parameters selection
Garin A.M., Vorobyev V.I.
Automated construction of a 3D plane model at the stage of technical proposals
Borgest N.M., Aleev R.H., Aksanian P.A., Gromov A.A.
Methodological support for the training of UAV designers and operators
Lukyanov O.E., Zolotov D.V.
Joint works of Ilyushin design bureau and general designer N. D. Kuznetsov
Novozhilov G.V.
Optimal command control of hypersonic aircraft flight path in conditions of atmospheric disturbances
Krikunov M.M.
Command control of hypersonic cruising aircraft during climb
Balakin V.L., Kotchyan A.G.
Disturbed motion of a hypersonic vehicle in climb
Balakin V.L., Krikunov M.M.
Theoretical and experimental analysis of the thermal state of transport aircraft compartments thermal state
Nikolayev V.N.
Analysis of control programs and flight paths of a hypersonic vehicle in climb
Balakin V.L., Krikunov M.M.
Assessing weight efficiency of carrier rockets launched from dirigibles and airplanes
Kurenkov V.I.
Design and technical characteristics of transport airplane for arctic exploration
Kuprikov N.V., Dolgov O.S., Kuprikov M.Y., Ivanov B.V.
Flight path of a supersonic aeroplane as the first stage of an aerospace system
Balakin V.L., Potapov V.I.
Parameters study in the electrothermal and jet protection of the airliner cockpit windows from fogging
Nikolayev V.N.
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