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Recuperative heat-exchange apparatus with porous metal for a liquid-propellant rocket engine
Authors: Pelevin F.V., Ponomarev A.V., Semenov P.Y. | Published: 16.06.2015 |
Published in issue: #6(663)/2015 | |
Category: Aviation, Rocket and Technology | |
Keywords: recuperative heat-exchange apparatus, porous mesh metal, inter-channel coolant transpiration, heat-exchange efficiency |
The Methodology of Selection of an Autoclave Barothermal Processing Mode for the Heat-Shield of Re-Entering Spacecraft
Authors: Tarasov V.A., Romanenkov V.A., Komkov M.A., Boyarskaya R.V. | Published: 28.09.2015 |
Published in issue: #9(666)/2015 | |
Category: Aviation, Rocket and Technology | |
Keywords: autoclave, heat-shielding, composite design, polymerization and viscosity binding, relationship between the continuous temperature change of a product and step change of the nitrogen pressure |
Research of the Capillary Phase Separator for Fuel Tanks of Liquid Propellant Rocket Engines at Evaporation of Cryogenic Components
Authors: Avraamov H.I., Pelevin F.V., Sapozhnikov V.B., Sintsov A.L. | Published: 29.10.2015 |
Published in issue: #10(667)/2015 | |
Category: Aviation, Rocket and Technology | |
Keywords: liquid propellant rocket engine, multiple launch, inter-tank device, capillary phase separator |
Special Features of Calculating the Composition and Temperature of Combustion Products of Superrich Oxygen-Methane Fuel
Authors: Dorofeev A.A., Yagodnikov D.A., Chertkov K.O. | Published: 29.10.2015 |
Published in issue: #10(667)/2015 | |
Category: Aviation, Rocket and Technology | |
Keywords: superrich oxygen-methane fuel, soot formation, chemical non-equilibrium, thermodynamic calculation, liquid propellant rocket engine, liquid gas generator |
The Role of the Capillary Pressure Component in the Displacement of Partially Wetting Liquid from the Capillary
Authors: Polyanskiy A.R., Romanov A.S., Semikolenov A.V. | Published: 20.11.2015 |
Published in issue: #11(668)/2015 | |
Category: Aviation, Rocket and Technology | |
Keywords: partially wetting liquid, meniscus, capillary, disjoining pressure, three phase contact, contact angle |
Numerical and Experimental Determination of the Optimal Length of Cylindrical Mixing Chamber of Supersonic Gas Ejector
Authors: Akimov M.V., Safargaliev T.D., Papyrin P.V. | Published: 20.11.2015 |
Published in issue: #11(668)/2015 | |
Category: Aviation, Rocket and Technology | |
Keywords: gas ejector, optimal length of a cylindrical mixing chamber, numerical calculation, critical operation |
The Influence of Magnetron Sputtering Conditions on the Structure of Heat Resistant ZrO2 Nanostructured Coatings
Authors: Valyukhov S.G., Stognei O.V., Filatov M.S. | Published: 20.11.2015 |
Published in issue: #11(668)/2015 | |
Category: Aviation, Rocket and Technology | |
Keywords: RF-magnetron sputtering, nanostructured films, stabilized zirconia dioxide, thermal annealing |
Stability of Parameters of Long Capillary Fuel Intake Devices Made of Combined Porous Mesh Metals
Authors: Novikov Y.M., Bolshakov V.A., Partola I.S. | Published: 20.11.2015 |
Published in issue: #11(668)/2015 | |
Category: Aviation, Rocket and Technology | |
Keywords: porous materials, porous metals, phase separator, capillary intake device, additional fuel tank, technological welding machine, maximum pore size, capillary holding capacity |
Analytic Hierarchy Process for Weight Coefficient Definition of Performance Function for Optimization of Hybrid Composite Wing for Reusable Space Vehicle
Authors: Pilyugina A.V., Ageyeva T.G. | Published: 20.11.2015 |
Published in issue: #11(668)/2015 | |
Category: Aviation, Rocket and Technology | |
Keywords: reusable space vehicle, hybrid composite materials, wing, multi-criteria optimization, analytic hierarchy process |
The Method of Experimental Research into the Efficiency of the Working Process in High Speed Solid Fuel Ramjet Engines
Authors: Aleksandrov V.Yu., Arefyev K.Yu., Prokhorov A.N., Fedotova K.V., Sharov M.S., Yanovskiy L.S. | Published: 11.02.2016 |
Published in issue: #2(671)/2016 | |
Category: Aviation, Rocket and Technology | |
Keywords: ramjet engine, afterburner, experimental study, combustion efficiency, specific impulse |