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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 23, No 3 (2024)

Selection of design parameters of a spacecraft electric propulsion engine ensuring the geostationary orbit raising mission

Kolesov A.V., Salmin V.V.

(Rus)

Vol 14, No 4 (2015)

Procedure of accomodation of earth remote sansing satellite external devices with regard for the satellite target operation

Akhmetov R.N., Shilov L.B., Kurenkov V.I., Yakischik A.A.

(Rus)

Vol 15, No 1 (2016)

Efficiency of using electric propulsion engines for the task of keeping in a near-circular orbit

Ishkov S.A.

(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 13, No 5-4 (2014): Special Issue

Calculation of sleeve-shaped filter elements made of the MR material

Zhizhkin A.M., Lazutkin G.V., Volkova T.V.

(Rus)

Vol 11, No 2 (2012)

Choice of design parameters of universal platforms of small space vehicles

Volotsuev V.V., Tkachenko I.S., Safronov S.L.

(Rus)

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

Correlation and regression model for the assessment of circular non-uniformity of the gas temperature field at the outlet of small gas turbine engine combustion chambers

Lukachev S.V., Abrashkin V.Y., Lansky A.M., Matveev S.G.

(Rus)

Vol 17, No 3 (2018)

Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines

Ryzhkov V.V., Morozov I.I.

(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 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 15, No 2 (2016)

Procedure of comparative assessment of the efficiency of Earth remote sensing satellites with different optoelectronic telescopic complexes

Stratilatova N.N., Kurenkov V.I., Kucherov A.S., Egorov A.S.

(Rus)

Vol 15, No 2 (2016)

Metodological basis of the development of a problem-oriented system for selecting design parameters of space vehicles

Stratilatov N.R., Kurenkov V.I., Kucherov A.S., Yakishik A.A.

(Rus)

Vol 13, No 4 (2014)

Choice of design characteristics of «garbage collector» spacecraft with a low-thrust electrojet engine

Ishkov S.A., Filippov G.A.

(Rus)

1 - 14 of 14 Items

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