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Space Energy, Power and Propulsion

Pequliarities of mathematical modeling of low-frequency dynamics of the staged liquid rocket sustainer engines at its startup

¹Pylypenko OV, ²Prokopchuk AA, ¹Dolgopolov SI, ²Pisarenko VYu., ²Kovalenko VN, ¹Nikolaev AD, ³Khoryak NV. Pequliarities of mathematical modeling of low-frequency dynamics of the staged liquid rocket sustainer engines at its startup. Space Science and Technology. 2017 ;23(5):03-13.

New method for the transformation of solar radiation energy into electric power for energy feeding of the space vehicles

¹Ludanov KI. New method for the transformation of solar radiation energy into electric power for energy feeding of the space vehicles. Kosm. nauka tehnol. 2007 ;13(6):031-038.

Experimental investigation of laboratory-scale rocket engine fed on solid polyethylene rod as fuel

¹Emets VV, ²Sanin FP, ³Dzhur Ye.O, ¹Masliany MV, ⁴Kostritsyn OU, ¹Minteev GV, ⁵Ushkanov VM. Experimental investigation of laboratory-scale rocket engine fed on solid polyethylene rod as fuel. Kosm. nauka tehnol. 2007 ;13(6):018-030.

The influence of electric energy disbalances on the spacecraft functionability under non-standard modes

¹Belov DG. The influence of electric energy disbalances on the spacecraft functionability under non-standard modes. Kosm. nauka tehnol. 2008 ;14(3):004-011.

Some methods for diagnostics of boundary conditions under ablation of thermal insulation surface with the use of fibre optical sensors

¹Gornostaev GF. Some methods for diagnostics of boundary conditions under ablation of thermal insulation surface with the use of fibre optical sensors. Kosm. nauka tehnol. 2010 ;16(4):46-50.

Characteristics of space debris-gatherers with electric propulsion at two variants of manoeuvres for their putting into demanded orbit

¹Dron NM, ²Dubovik LG, ¹Kondratyev AI, ¹Khitko AV, ²Horolsky PG. Characteristics of space debris-gatherers with electric propulsion at two variants of manoeuvres for their putting into demanded orbit. Kosm. nauka tehnol. 2010 ;16(5):59-61.

Reliability analyses of solar panel drive for long lifetime spacecrafts

¹Shatikhin VE, ²Semenov LP, ³Makarov AL, ³Khoroshylov VS, ⁴Popel′ VM, ⁵Ignatovich SR. Reliability analyses of solar panel drive for long lifetime spacecrafts. Kosm. nauka tehnol. 2010 ;16(5):54-58.

The influence of concentrator geometry on the energy parameters of the reception system of the space solar power plant

¹Knysh LI. The influence of concentrator geometry on the energy parameters of the reception system of the space solar power plant. Kosm. nauka tehnol. 2011 ;17(5):19-23.

Power losses for solar arrays of a spacecraft in the Earth’s polar ionosphere and magnetosphere

¹Shuvalov VA, ¹Pismennyi NI, ²Kochubey GS, ³Nosikov SV. Power losses for solar arrays of a spacecraft in the Earth’s polar ionosphere and magnetosphere. Kosm. nauka tehnol. 2011 ;17(3):05-15.

Dynamics of the composite casing of solid-propellant rocket engine under the influence of impulse loads describing the work processes in the engine

¹Chernobryvko MV, ¹Avramov KV, ²Degtyarenko PG, Tonkonogenko AM, ³Mesha YV, ⁴Tishkovets OV, ⁴Zholos OV. Dynamics of the composite casing of solid-propellant rocket engine under the influence of impulse loads describing the work processes in the engine. Kosm. nauka tehnol. 2017 ;23(1):18-29.

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