Ageenko, Y. I.

Issue Section Title Abstract 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 Abstract 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 Abstract 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 Abstract 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 Abstract 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 Abstract 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 Abstract 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 Abstract PDF
(Rus)

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies