Search by keyword: "spacecraft"
Calculation of the Refueling Dose of a Temperature Control System with the Two-Phase Circuit
| Authors: Borshchev N.O. | Published: 10.01.2024 |
| Published in issue: #4(147)/2023 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: loop heat pipe, thermal balance, thermal control system, spacecraft | |
The Concept of Constructing a Stand to Test the SpaceWire Onboard Equipment with Possibility of Software and Hardware Simulation of Reconfigurable Topology of the Spacecraft Onboard Network
| Authors: Maksyutin A.S., Murygin A.V. | Published: 23.06.2023 |
| Published in issue: #2(145)/2023 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: test stands, test methods, spacecraft, onboard networks, SpaceWire | |
Influence of Spacecraft Surface Spectral Radiation Characteristics on the Accuracy of Thermal Load Simulations in Infrared Simulators
| Authors: Kolesnikov A.V., Paleshkin A.V., Pronina P.F., Shemetova E.V. | Published: 01.04.2022 |
| Published in issue: #1(140)/2022 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: spacecraft, thermal tests, external thermal loads, spectral errors, infrared radiation sources | |
Error Inherent in Simulating Planetary Thermal Effect on the Spacecraft Surface by using Isotropic Planetary Radiation Intensity Field Model Instead of Anisotropic
| Authors: Kolesnikov A.V., Pronina P.F., Paleshkin A.V. | Published: 23.12.2020 |
| Published in issue: #6(135)/2020 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: planet, radiation, radiation intensity field model, heat flux, angle factor, radiation field simulation, spacecraft | |
Technique Employing Topology Optimisation to Determine Panel-to-Panel Support Bracket Positions in a Spacecraft Body
| Authors: Borovikov A.A., Leonov A.G., Tushev O.N. | Published: 03.09.2019 |
| Published in issue: #4(127)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: topology optimisation, finite element method, dynamic compatibility, spacecraft, technique | |
Performance of a Solar Thermal Propulsion Featuring Latent Heat Storage and Subsequent Hydrogen Burning
| Authors: Finogenov S.L., Kolomentsev A.I. | Published: 02.08.2018 |
| Published in issue: #4(121)/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, spacecraft, geostationary orbit | |
Performance of a Solar Thermal Propulsion Featuring Latent Heat Storage and Subsequent Hydrogen Burning
| Authors: Finogenov S.L., Kolomentsev A.I. | Published: 02.08.2018 |
| Published in issue: #4(121)/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, spacecraft, geostationary orbit | |
Thermal Loading Simulators with Diffuse Emitter Modules Operating over a Strictly Bounded Solid Angle
| Authors: Kolesnikov A.V., Paleshkin A.V., Shemetova E.V. | Published: 02.08.2018 |
| Published in issue: #4(121)/2018 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: simulation, thermal loading, spacecraft, radiation phase function, diffuse radiation | |
Thermal Loading Simulators with Diffuse Emitter Modules Operating over a Strictly Bounded Solid Angle
| Authors: Kolesnikov A.V., Paleshkin A.V., Shemetova E.V. | Published: 02.08.2018 |
| Published in issue: #4(121)/2018 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: simulation, thermal loading, spacecraft, radiation phase function, diffuse radiation | |
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 | |