Author Details

Агеенко, Ю. И., Конструкторское бюро химического машиностроения им. А.М. Исаева - филиал ФГУП ГКНПЦ им. М.В. Хруничева, Russian Federation

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 8, No 3-2 (2009): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING 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 PDF
(Rus)
Vol 11, No 3-1 (2012): Special Issue CONFERENCE MATERIALS Investigation of the possibility of the creation LREST by thrust 400 N with a baffle - centrifugal scheme of NT and NDMG mixing 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 5-1 (2014): Special Issue ISSUE WITHOUT SECTION 50 n thrust correction engine for the "Luna-resurs" lunar module descent engine PDF
(Rus)
Vol 13, No 5-1 (2014): Special Issue ISSUE WITHOUT SECTION Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency PDF
(Rus)
Vol 13, No 5-3 (2014): Special Issue ISSUE WITHOUT SECTION Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel PDF
(Rus)
Vol 13, No 5-3 (2014): Special Issue ISSUE WITHOUT SECTION Verification of energy efficiency of a low-thrust liquid-propellant engine with the deflector-centrifugal injecting pattern PDF
(Rus)

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