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GEOSTATIONARY SPACECRAFT ORBIT SLAVING AND MANEUVER: THRUSTERS ON DRIVES INSTALLATION SCHEME
Ermoshkin Y.M., Raevskiy V.A., Urusov V.M., Yermoshkin Y.M., Raevsky V.A., Urusov V.M.
Development of the two-fuel combustion chamber and calculation of processes for the theory of turbulent burning
Baklanov A.V.
NANOMETALLIC FUEL FOR THE ROCKET ENGINES
Krushenko G.G.
Verification of thermodynamic parameters of a mixture of generator gas on oxygen-hydrogen fuel with an excess of one of the fuel components
Belyakov V.A., Vasilevsky D.O., Maslov D.V., Kilyashov A.A., Romashko R.V.
The possibility of using methane-hydrogen fuel in converted gas turbine engines for power plants
Baklanov A.V.
RESEARCH OFEFFICIENCYOFELECTROHYDRAULIC EFFECTSAT RECEPTIONCAVITATIONWATER-COALOF FUEL FOR BOILER INSTALLATIONSOF KRASNOYARSK REGION
Dubrovskiy V., Isakov Y.V., Potylitsyn M.Y., Potapov I.I., Shirokov V., Dubrovsky V.A., Isakov Y.V., Potilicyn M.Y., Potapov I.I., Shirokov V.N.
SUPERDISPERSED ALUMINUM AS HIGH-ENERGY FUEL
Krushenko G.G.
CRITERIAOF ORBITALCONTROLTHRUSTER OPTIMALALLOCATIONON BOARD OFGEOSTATIONARY SPACECRAFT
Ermoshkin Y.M., Urusov V.M., Yermoshkin Y.M., Urusov V.M.
ADJUSTMENT OF POWER PERFORMANCES OF PROPELLANT BASED ON AMMONIUM NITRATE
Gorbenko T.I.
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