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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 |