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Design of a Heat Transfer Intensification System for Hydrocarbon Fuel in the Cooling Channels of the Liquid Rocket Engine
| Authors: Yusha V.L., Chernov G.I., Shcherban K.V. | Published: 06.09.2018 |
| Published in issue: #8(701)/2018 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: liquid rocket engine, strength analysis, thermal analysis, hypersonic aircraft, cooling system, heat transfer intensification systems |
A Comparison of Characteristics of a Model of the Anode Layer Thruster Operating on Xenon, Argon and Nitrogen
| Authors: Dukhopelnikov D.V., Ryаzanov V.A., Shilov S.O. | Published: 26.07.2018 |
| Published in issue: #7(700)/2018 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: electric rocket propulsion unit, anode layer thruster, reactive gas, ambient air, ion current, power thrust ratio |
The Methods of Designing a Polymer Composite Wing Using Parametrical Modeling. Part III. Selection and Justification of Optimal Schemes for Reinforcing Load Bearing Elements
| Authors: Mikhailovskiy K.V., Baranovski S.V. | Published: 31.05.2018 |
| Published in issue: #5(698)/2018 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: airliner, wing, structural arrangement, carbon fibre, reinforcement pattern |