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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 |
About features of use of electrorocket impellent installations for transportation of radio nuclides in distant space
| Authors: Dmitriev S.N., Aliev I.N., Onufriev A.V. | Published: 30.07.2013 |
| Published in issue: #2(611)/2011 | |
| Category: Transportation and Power Engineering | |
| Keywords: spacecraft, electrical rocket thruster, power plant, heat radiator, radioactive isotope, thermoelectric generator, characteristic velocity, specific impulse, the time of orbital flight, specific mass, electrical power, specific thermal power, initial mass, payload, the share of payload, propellant |