Author Details

Nigodjuk, V. E.

Issue	Section	Title	File
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	(Rus)
Vol 11, No 3-3 (2012): Special Issue	CONFERENCE MATERIALS	Ways to improve the workflow of liquid rocket thrusters on hypergolic propellants	(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	(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	(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	(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	(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	(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	(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	(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	(Rus)

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