Transfer of a Satellite from High Elliptical to Geostationary Orbit with the Help of Electric Propulsion
| Autor: | A.A. Kvetkin, V. V. Salmin, K.V. Petrukhina |
|---|---|
| Rok vydání: | 2017 |
| Předmět: |
Physics
020301 aerospace & aeronautics Geostationary transfer orbit business.industry 02 engineering and technology General Medicine Graveyard orbit 01 natural sciences 010305 fluids & plasmas 0203 mechanical engineering Electrically powered spacecraft propulsion 0103 physical sciences Geostationary orbit Apogee kick motor Satellite Orbit (control theory) Aerospace engineering Orbit insertion business |
| Zdroj: | Procedia Engineering. 185:352-358 |
| ISSN: | 1877-7058 |
| DOI: | 10.1016/j.proeng.2017.03.315 |
| Popis: | This paper considers a combined scheme of insertion of a satellite into a geostationary orbit with the help of high and low torque thrusters. The start orbit is high elliptical and is formed by the third stage of the launch vehicle. Further insertion is performed by an electric propulsion unit. The trajectory of insertion, transfer time and propellant mass have been calculated. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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