CONTENTS
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Optimization of pin injector elements for combustion chamber of powerful liquid rocket engine A.S.Kiselev ………………………..…
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4
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Three-dimensional calculation of gas-dynamic parameters of combustion products in annular chamber of liquid rocket engine with rotating detonation V.K.Chvanov, V.A.Levin, P.S.Levochkin, I.S.Manuilovich, V.V.Markov, L.E.Sternin ………………………
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23
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The layout schemes of perspective launch-vehicles, equipped with multi-chamber propulsion systems and composite nozzle blocks with autoregulation V.K.Chvanov, A.G.Gonchar, A.N.Kraiko, P.S.Levochkin, V.M.Nizovtsev, N.B.Ponomarev, K.S.P’yankov, V.K.Starkov, L.E.Sternin, N.I.Tillyaeva Н.И. Тилляева, V.E.Shirshov, A.E.Denisov, V.Y.Yuriev …………………..……….…...
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36
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Operator’ interface of system of functional diagnostics of LRE V.T.Bukanov, S.A Dichev, D.S.Martirosov …………………………...
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65
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Mathematical model of dynamic processes of pressure stabilizer of powerful liquid rocket engines B.M.Gromyko, I.M.Koshelev, E.V.Krapivnykh ………….….……………………………………...
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75
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Application of calculation-experimental model for forecast of parameters of operational processes of LRE in cycle of repeated fire tests V.T.Bukanov, S.S.Kamensky, D.S.Martirosov ….…………...
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91
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Creation of RD181 LRE Y.Y.Ivanov, M.Y.Ivanov……..…………...
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100
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Experimental study of laser ignition of oxygen-kerosene propellant in LRE chambers V.K.Chvanov, I.A.Ganin, N.G.Ivanov,
P.S. Levochkin, E.N.Romasenko, B.A.Surkov ……………………..
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113
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Heat exchangers of RD119 engine of “Cosmos” launch-vehicle. O.G.Klyueva …………….…………………………………………...……
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134
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Results of autonomous development of improved pressurization unit. O.G.Klyueva …………………….…………..……..….……….…..
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151
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Research and development of new version of a lift-off seal of oxidizer pump of RD191 engine. A.T.Grebenyuk, N.P.Poletaev, E.N.Romasenko, D.A.Sazonov ………………………………………...
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163
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Experimental estimation of influence of design parameters of pressure stabilizer on it static characteristics and operability. B.M.Gromyko, E.V.Krapivnykh, A.A.Telenkov, A.A.Tyurin .……….
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181
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About some features of temperature distribution in design of LRE during brazing. A.B.Aminov, K.E.Dubrovsky …………………..……..
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198
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Determination of thickness of silver coating by method of X-ray fluorescence analysis. A.M.Polyansky, A.N.Vycherov, V.M.Polyansky, E.V.Voronkova, N.G.Maslov …….………….……..
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211
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Causes of premature destruction of fuel pump casings of AK9ч alloy during hydrostatic tests. A.M.Polyansky, V.M.Polyansky ...…..
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226
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Ensuring operational characteristics of turbines of TPU at its work in composition of LRE. Y.I.Kanalin, I.A.Chernysheva ………..……
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237
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About problems with use of high-strength alloys in oxidizer pump impeller of LRE. E.V.Voronezhsky, L.I.Kozhemyakin, V.I.Novikov...
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263
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Automated complex of testing of thickness of technological coatings of LRE elements. A.V.Barinov, D.S.Sergeev, I.Y.Kinzhagulov, A.A.Smirnov, K.A.Stepanova, V.A.Kaloshin, A.M.Perfilov, A.S.Machikhin ………………..………….……………..………………..
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275
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Research and adaptation of electromagnetic method to determination of thickness of metal-ceramic coatings. E.V.Gnutenko, V.A.Kaloshin, A.P.Kren, V.A.Rudnitsky ………………………..……...
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289
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Control subsystem of stand systems of LRE emergency protection. I.B.Davydov ……………..…………………………….….………………..
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299
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Simulation subsystem of stand system of LRE emergency protection. I.B.Davydov, V.V.Mozdakov……………..….……………………..
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307
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Subsystem of automated workplace of operator of stand LRE emergency protection system. I.B.Davydov, A.A.Plato ………….………..
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314
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Onboard LRE emergency protection system of advanced LV. I.B.Davydov ………….……………..…………………….………………..
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323
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Determination of density of RP-1, T-6 and RG-1 fuels in LRE working ranges of temperatures and pressures. A.N.Kolymagin …....
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335
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Rakhmanin Vyacheslav Fedorovich. To 80th birthday anniversary (biographic article) …….………………………………………..…..
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353
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Our “Proceedings” ………………………………………………….
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369
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374
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