Insertion into Geostationary Orbit of a Spacecraft with Diffractive Orbit by Low Torque Electric Propulsion
| Autor: | V.A. Soyfer, V. V. Salmin, Sergey V. Karpeev, A. S. Chetverikov, I. S. Tkachenko, K. V. Peresypkin |
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| Rok vydání: | 2017 |
| Předmět: |
Physics
Geostationary transfer orbit business.industry 02 engineering and technology General Medicine Graveyard orbit 01 natural sciences Orbital station-keeping 010309 optics Synchronous orbit Physics::Space Physics 0103 physical sciences 0202 electrical engineering electronic engineering information engineering 020201 artificial intelligence & image processing Apogee kick motor Astrophysics::Earth and Planetary Astrophysics Aerospace engineering Orbital maneuver Orbit insertion business Medium Earth orbit |
| Zdroj: | Procedia Engineering. 185:332-337 |
| ISSN: | 1877-7058 |
| Popis: | The paper solves the problem of control over and insertion into geostationary orbit of a spacecraft with diffractive optical elements with the help of low torque electric propulsion (EP). Main features of a design layout of a spacecraft with diffractive optics and the requirements for inserting such spacecraft into geostationary orbit are discussed. The prototype of such system is the MOIRE project spacecraft. The paper suggests a three-stage ballistic insertion scheme: lifting to near Earth orbit by a launch vehicle, transfer to intermediate orbit with the help of acceleration module, and at the final stage the spacecraft is transferred from intermediate to geostationary orbit by low thrust electric propulsion system. |
| Databáze: | OpenAIRE |
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