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Vol 23, No 1 (2024)

Reducing energy consumption of vertical take-off and landing unmanned aerial vehicle using hybrid technical solutions

Lukyanov O.E., Hoang V.H., Komarov V.A., Nazarov D.V., Kurkin E.I., Quijada Pioquinto J.G., Chertykovtseva V.O.

(Rus)

Vol 10, No 3-3 (2011): Special Issue

Heat engine cycle limitations imposed by fuel properties

Mikheyenkov E.L.

(Rus)

Vol 12, No 4 (2013)

Spacecraft preset orbital parameters control by means of thrusters

Salmin V.V., Volotsuev V.V., Shikhanov S.V.

(Rus)

Vol 10, No 5 (2011)

Vortex gas wind-driven power plant for supplying compressor stations with electrical energy

Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.

(Rus)

Vol 12, No 3-1 (2013): Vestnik SSAU

Limit values of the Brayton cycle with the use of reduced fuel characteristics

Mikheenkov E.L., Nekrasova S.O.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

Selection of optimal configuration and workflow parameters of autonomous micro gas turbine plant

Baturin O.V., Smirnova Y.D.

(Rus)

Vol 11, No 5-1 (2012): Special Issue

Vortical gaz-wind-energy plant

Biryuk V.V., Zubrilin I.A., Krasnorutskiy A.S.

(Rus)

Vol 21, No 3 (2022)

Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle

Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.

(Rus)

Vol 17, No 3 (2018)

Schemes, parameters, work process, characteristics and structure of long-range interception aircraft engines

Kovalev A.V., Sanin V.N., Krivenok A.G., Korolenko V.V.

(Rus)

Vol 10, No 6 (2011)

Planning a factorial experiment for testing a single-stage ultralow power turbine

Grigoryev V.A., Radko V.M., Kalabukhov D.S.

(Rus)

Vol 12, No 2 (2013)

Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200

Ageenko Y.I., Nigodyuk V.E., Ryzhkov V.V., Sulinov A.V., Shustov S.A.

(Rus)

1 - 11 of 11 Items

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