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Comparative evaluation of the effectiveness of the application of perspective types of electric propulsion thrusters in the small spacecraft
- Authors: Kulkov V.M.1, Obukhov V.A.1, Yegorov Y.G.1, Belik A.A.1, Krainov A.M.2
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Affiliations:
- Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)
- Scientific-Production Association named after S. A. Lavochkin, Moscow
- Issue: Vol 11, No 3-1 (2012): Special Issue
- Pages: 187-195
- Section: CONFERENCE MATERIALS
- URL: https://journals.ssau.ru/vestnik/article/view/2115
- DOI: https://doi.org/10.18287/2541-7533-2012-0-3-1(34)-187-195
- ID: 2115
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Abstract
The report includes comparative analysis of efficiency in the use of small spacecraft with electric propulsion based on ion thrusters, stationary plasma thrusters and pulsed plasma thrusters.
About the authors
V. M. Kulkov
Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)
Author for correspondence.
Email: riame@sokol.ru
Candidate of Engineering Science
Senior Researcher, Head of Department
Russian FederationV. A. Obukhov
Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)
Email: riame@sokol.ru
Candidate of Engineering Science
Senior Researcher, Vice Director
Russian FederationY. G. Yegorov
Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)
Email: riame@sokol.ru
Designer
Russian FederationA. A. Belik
Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)
Email: riame@sokol.ru
Candidate of Engineering Science
Senior Researcher, Head of Sector
Russian FederationA. M. Krainov
Scientific-Production Association named after S. A. Lavochkin, Moscow
Email: ztk-tol@mail.ru
Senior Specialist
Russian FederationReferences
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