Erscheint 6 Ausgaben pro Jahr
ISSN Druckformat: 1948-2590
ISSN Online: 1948-2604
EXPERIMENTAL MODEL STUDIES OF THE EFFECTS OF JET FLOWS ON THE LAUNCH VEHICLE AND LAUNCH PAD WITH A SHORT EXHAUST CHANNEL
ABSTRAKT
This article presents the results of experimental model studies of gas-dynamic, thermal, and acoustic loads on the elements of a launch vehicle and launch pad when using the CX-36 launch complex with a short exhaust channel. The data obtained to date are of significant interest to specialists in the field of space rocket engineering.
-
Antokhin, P.S., Arykhov, Yu.B., Ganabov, V.I., Gusev, V.P., Drozdov, S.M., Zhilin, Yu.V., Zhirnikov, B.L., Ivanov, A.N., Kazanskii, R.A., Krokhin, A.S., Kudin, O.K., Leites, E.A., Loboda, V.L., Marushkin, M.F., Nesterov, Yu.N., Pokhvalinskii, S.M., Stolyarov, E.P., and Shamshurin, A.A., Model Experimental Studies of Gasdynamics, Heat Transfer and Acoustics under Impact of High Temperature Jets of Rocket Engines on a Launch Facility with an Exhaust Channel, Trudy TsAGI, no. 2786, 2019.
-
Petrov, G.I., Likhushin, V.Ya., Nekrasov, I.P., and Sorkin, L.I., Viscosity Effect on a Supersonic Flow with Shock Waves, Trudy CIAM, no. 224, 1952.
-
Lipnitskiy, Yu.M. and Safronov, A.V., Ground Testing of the Launch Vehicle Acoustics, TsAGI Sci. J., vol. 45, nos. 3-4, pp. 237-254,2014.