Author Details

Нигодюк, В. Е.

Issue Section Title File
Vol 12, No 2 (2013) AIRCRAFT AND SPACE ROCKET ENGINEERING Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200 PDF
(Rus)
Vol 5, No 2-2 (2006): Special Issue TECHNICAL SCIENCES Interaction of drops of a plume of a liquid with heated granulouse units PDF
(Rus)
Vol 5, No 2-2 (2006): Special Issue TECHNICAL SCIENCES The concept and the results of elaboration of the automated test bench for testing the rocket engine PDF
(Rus)
Vol 8, No 3-2 (2009): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Features of calculation of hydraulic characteristics of capillary spray jets of is liquid-stnyh rocket engines of small pull-rod PDF
(Rus)
Vol 8, No 3-2 (2009): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING The flowing reactor as the tool of an experimental research of processes of transformation self-igniting liquid rocket fuel PDF
(Rus)
Vol 8, No 3-2 (2009): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Research of laws of interaction of components in a liquid phase self-igniting liquid rocket fuel PDF
(Rus)
Vol 11, No 3-3 (2012): Special Issue CONFERENCE MATERIALS Ways to improve the workflow of liquid rocket thrusters on hypergolic propellants PDF
(Rus)
Vol 11, No 3-3 (2012): Special Issue CONFERENCE MATERIALS Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block PDF
(Rus)
Vol 13, No 5-2 (2014): Special Issue ISSUE WITHOUT SECTION Automated thermovacuum firing test facility for testing and research of workflow in low-thrust rocket engine on hypergolic propellants PDF
(Rus)
Vol 13, No 5-2 (2014): Special Issue ISSUE WITHOUT SECTION Investigation of transformation of intermediate products of liquid-phase interaction propellant at the onset of combustion for rocket engine PDF
(Rus)
Vol 15, No 4 (2016) AIRCRAFT AND SPACE ROCKET ENGINEERING Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines PDF
(Rus)
Vol 15, No 4 (2016) AIRCRAFT AND SPACE ROCKET ENGINEERING Peculiarities of the working process of low-thrust hypergolic-propellant liquid rocket engines with a thrust of less than 1 N PDF
(Rus)
Vol 10, No 3-3 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Investigation of the kinetic properties of gas products of liquid-phase interaction hypergolic liquid rocket fuel PDF
(Rus)
Vol 10, No 3-3 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Increasing the energy efficiency of liquid rocket engine of small thrust (0,1-1,0) N with jet scheme of mixing PDF
(Rus)
Vol 10, No 3-3 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Influence in a constructive and regime parameters antechamber by operation-in the combustion chamber liquid-propellant rocket engine thrusters on hypergolic liquid propellants PDF
(Rus)

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