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Motion Control of Electric Propulsion Spacecraft Transfers between the Libration Points L1 and L2 of the Earth–Moon System
| Authors: Fain M.K., Starinova O.L. | Published: 26.11.2019 |
| Published in issue: #11(716)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: spacecraft, low thrust engine, sequential linearization method, Earth–Moon system, libration point |
Methods of Calculation of Performance Indicators of Spacecraft Flight Control Systems
| Authors: Panteleymonov I.N., Potyupkin A.Y., Trankov V.M., Panteleymonova A.V., Filatov V.V., Todurkin V.V. | Published: 26.11.2019 |
| Published in issue: #11(716)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: communication and control session, spacecraft, mission control center, flight control system, command-measuring station, on-board equipment |
The Concept of Generalization of Structural Properties of Measuring Tasks when Providing Navigation and Ballistic Support for Spacecraft
| Authors: Betanov V.V., Koryanov V.V. | Published: 26.07.2018 |
| Published in issue: #7(700)/2018 | |
| Category: Aviation, Rocket and Technology | Chapter: Inspection and Testing of Aircraft and Aircraft Systems | |
| Keywords: measuring task, complex dynamic object, object-system, generalized observability, spacecraft, navigation and ballistic support |
Deploying a Planar Elastic Rod System with Cable Elements Attached to a Spacecraft
| Authors: Russkikh S.V. | Published: 28.04.2018 |
| Published in issue: #4(697)/2018 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: elastic systems dynamics, spacecraft, mobile coordinate system, elastic-viscous nodal hinges, tensile cable, rod system deployment |
Simulation of a Spacecraft Landing Using a Landing Device with Crash Legs
| Authors: Lukovkin R.O., Shcheglov G.A. | Published: 19.12.2017 |
| Published in issue: #12(693)/2017 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: spacecraft, landing gear, crash leg, crash box, energy absorption, numerical simulation |
A New Approach to Measure Spacecraft Moments of Inertia Based on the Analysis of a Self-Oscillating System
| Authors: Reznik S.V., Videnkin N.A. | Published: 07.09.2016 |
| Published in issue: #9(678)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: moment of inertia, spacecraft, self-oscillations |
Thermal regulation system of an orbital manned spacecraft with a vapor compression refrigerating machine
| Authors: Smorodin A.I., Men, Garanov S.A. | Published: 13.11.2014 |
| Published in issue: #11(656)/2014 | |
| Category: Calculation and Design of Machinery | |
| Keywords: turbo-compressor, heat exchanger, refrigerant, life support system, thermal control system, spacecraft, vapor compression refrigerating cycle. |
Experimental and computational studies of the response of a radioactive waste ampoule shell model to an external harmonic action allowing for heat release
| Authors: Onufriev A.V., Dmitriev S.N., Onufriev V.V. | Published: 08.09.2014 |
| Published in issue: #9(654)/2014 | |
| Category: Transportation and Power Engineering | |
| Keywords: spacecraft, radioactive waste, elastic dynamic properties, ampoule, self-delivery |
Technical aspects of designing a spacecraft for transporting radioactive waste
| Authors: Onufriev A.V., Dmitriev S.N., Onufriev V.V. | Published: 01.08.2014 |
| Published in issue: #8(653)/2014 | |
| Category: Transportation and Power Engineering | |
| Keywords: spacecraft, nuclear waste, configuration, ballistic design, mass analysis, design arrangement, load bearing structure, finite element model, self-delivery |
Technical aspects of designing a spacecraft for transporting radioactive waste
| Authors: Onufriev A.V., Dmitriev S.N., Onufriev V.V. | Published: 07.05.2014 |
| Published in issue: #5(650)/2014 | |
| Category: Technology and Process Machines | |
| Keywords: spacecraft, nuclear waste, ballistic properties, mass properties, power plant, electric propulsion, design arrangement, structural frame, self-delivery |