Radiation Heat Transfer and Thermal Protection of Air-Gas Channel of Gas Dynamic Plant
Authors: Tovstonog V.A. | Published: 05.12.2017 |
Published in issue: #6(117)/2017 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: gas dynamic installation, high temperatures, radiation heat transfer, thermal protection |
Optimization of Hybrid Composite Material Structure for Wing Skin of Tourist Class Reusable Space Vehicle
Authors: Ageeva T.G., Ashikhmina E.R., Prosuntsov P.V. | Published: 09.02.2018 |
Published in issue: #1(118)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: reusable space vehicles, space tourism, hybrid polymer composite materials, wing |
Method for Splitting into Physicall Processes in Task of the Flow Over a Perspective High-Speed Vehicle Modelling
Authors: Yatsukhno D.S., Surzhikov S.T. | Published: 09.02.2018 |
Published in issue: #1(118)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: splitting methods, hypersonic vehicle aerothermodynamics, unstructured grids, stream surface, aerodynamic design |
Computational and Experimental Technique for Selecting Chamber Parameters for Thermal Condition Testing of Onboard Equipment in Unpressurised Spacecraft
Authors: Alekseev V.A., Kudryavtseva N.S., Titova A.S. | Published: 09.04.2018 |
Published in issue: #2(119)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: spacecraft, temperature control systems, thermal vacuum chamber, climate chamber, onboard equipment, unpressurised compartment, Electronic and Electromechanical (EEE) parts |
Estimating Feasibility of Taking Quadratic Terms into Account During Guidance Error Analysis for the Case of Interplanetary Spacecraft
Authors: Sukhova S.V. | Published: 10.04.2018 |
Published in issue: #2(119)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
Keywords: guidance error analysis, Monte Carlo method, interplanetary transfer |
Analysing Specifics of Manufacturing Items out of Polymer Composite Materials by Means of Filament Winding. Shaping Mandrels
Authors: Zuev A.S., Emashev A.Yu., Shaydurova G.I.  | Published: 14.06.2018 |
Published in issue: #3(120)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
Keywords: filament winding, reinforcement, matrix, mandrel, deformation, heat setting |
Estimating Thermal Decomposition Parameters for Lithium Hydride in a High Temperature Gas Flow
Authors: Tovstonog V.A. | Published: 14.06.2018 |
Published in issue: #3(120)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
Keywords: lithium hydride, high temperature gas flow, heat-absorbing material, thermal decomposition, ablation, decomposition parameters |
Solar Thermal Propulsion Concept Featuring Phase-Change Latent Heat Storage and Subsequent Hydrogen Burning in Fluorine
Authors: Finogenov S.L. | Published: 14.06.2018 |
Published in issue: #3(120)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Innovation Technologies of Aerospace Engineering | |
Keywords: solar thermal propulsion, latent heat storage, phase-change materials, subsequent hydrogen burning, fluorine, spacecraft, geostationary orbit, spa-cecraft |
Investigating Various Ways of Cooling Cryogenic Fuel Tanks of Aerospace Equipment
Authors: Yuranev O.A. | Published: 14.06.2018 |
Published in issue: #3(120)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Innovation Technologies of Aerospace Engineering | |
Keywords: cryogenic fuel tanks, cooling, liquid nitrogen, liquid hydrogen, liquid oxygen, gaseous helium, liquid oxygen |
Optimum Anisotropic Coating Thickness for a Wall Separating Two Different Media and Subjected to Local Heating
Authors: Attetkov A.V., Volkov I.K. | Published: 02.08.2018 |
Published in issue: #4(121)/2018 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts | |
Keywords: isotropic separator wall, anisotropic coating, local heating, steady-state temperature field, optimum coating thickness |