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Title
Authors
Vol 23, No 1 (2024)
Optimization of trajectory motion of the first stage of an aerospace system
Khramov A.A.
PDF
(Rus)
Vol 17, No 4 (2018)
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
PDF
(Rus)
Vol 10, No 3-2 (2011): Special Issue
Design procedure of fundamental parameters of the direct-flow detonation pulsing engine
Porshnev V.A.
PDF
(Rus)
Vol 9, No 2 (2010): Special Issue
Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust
1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1.
PDF
(Rus)
Vol 16, No 3 (2017)
Locally optimal control of space tug motion between the libration points of the Earth-Moon system
Starinova O.L., Fain M.K.
PDF
(Rus)
Vol 13, No 5-1 (2014): Special Issue
Experimental verification of the possibility of improving the liquid propelant rocket engine performance for the “Vega” launcher upper stage
Kovalenko A.N., Pereverzev V.G., Marchan R.A., Blishun Y.V.
PDF
(Rus)
Vol 10, No 3-4 (2011): Special Issue
Aspects of the numerical method calculating thermogazodynamic lrest based on not perfect passing of workflows in the combustion chamber
Silyutin M.V., Shustov S.A.
PDF
(Rus)
Vol 8, No 3-3 (2009): Special Issue
Development of advanced low thrust rocket engines with ecologically friendly propellants
1 1., 1 1., 1 1.
PDF
(Rus)
Vol 10, No 3-3 (2011): Special Issue
Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants
Silyutin M.V., Shustov S.A.
PDF
(Rus)
Vol 12, No 4 (2013)
The usage of high power supply capacity transport spacecraft
Ivanovich S.N.
PDF
(Rus)
Vol 10, No 3-2 (2011): Special Issue
The numerical modelling of processes in combustion chambers of low thrust rocket engines
Salich V.L.
PDF
(Rus)
Vol 10, No 6 (2011)
Estimation of the required thrust impulse for small spacecraft (SSC) control system with a propulsion system using fuel gas components
Titov B.A., Koltsov I.V.
PDF
(Rus)
Vol 10, No 1 (2011)
Optimal program of controlling continuous low thrust in the flight between noncoplanar elliptical and geostationary orbits
Fadeenkov P.V., Ishkov S.A.
PDF
(Rus)
Vol 8, No 3-3 (2009): Special Issue
Oxyhydrogen propulsion device base on water electrolysis and lrest on component H2 + O2 for control system SS
1 1., 1 1., 1 1., 1 1., 1 1.
PDF
(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.
PDF
(Rus)
Vol 10, No 3-3 (2011): Special Issue
Research of the possibility of thermal conditions LREST using an infrared thermal imaging system
Ryzhkov V.V., Silyutin M.V.
PDF
(Rus)
Vol 8, No 3-2 (2009): Special Issue
Mixing parameters investigations and methods of approach to calculations and development of the thrusters with a spray-centrifugal scheme of NT and NDMH mixing on the confusion chamber wall in considered
1 1.
PDF
(Rus)
1 - 17 of 17 Items

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