Optimization of the trajectory of the spacecraft insertion into the system of heliocentric orbits
The possibility of the spacecraft insertion into the system of operational heliocentric orbits has been analyzed. It has been proposed to use a system of several operational heliocentric orbits. On each orbit, the spacecraft makes one or more revolutions around the Sun. These orbits are characterize...
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Veröffentlicht in: | Cosmic research 2017-05, Vol.55 (3), p.214-223 |
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description | The possibility of the spacecraft insertion into the system of operational heliocentric orbits has been analyzed. It has been proposed to use a system of several operational heliocentric orbits. On each orbit, the spacecraft makes one or more revolutions around the Sun. These orbits are characterized by a relatively small perihelion radius and relatively high inclination, which allows one to investigate the polar regions of the Sun. The transition of the spacecraft from one orbit to another has been performed using an unpowered gravity assist maneuver near Venus and does not require the cruise propulsion operation. Each maneuver transfers the spacecraft into the sequence of operational heliocentric orbits. We have analyzed several systems of operational heliocentric orbits into which the spacecraft can be inserted by means of the considered transportation system with electric propulsion (EP). The mass of the spacecraft delivered to these systems of operational orbits has been estimated. |
doi_str_mv | 10.1134/S0010952517020034 |
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We have analyzed several systems of operational heliocentric orbits into which the spacecraft can be inserted by means of the considered transportation system with electric propulsion (EP). 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We have analyzed several systems of operational heliocentric orbits into which the spacecraft can be inserted by means of the considered transportation system with electric propulsion (EP). The mass of the spacecraft delivered to these systems of operational orbits has been estimated.</description><subject>Astronomy</subject><subject>Astrophysics and Astroparticles</subject><subject>Astrophysics and Cosmology</subject><subject>Electric propulsion</subject><subject>Inclination</subject><subject>Orbit insertion</subject><subject>Orbits</subject><subject>Physics</subject><subject>Physics and Astronomy</subject><subject>Polar environments</subject><subject>Polar regions</subject><subject>Solar orbits</subject><subject>Space Exploration and Astronautics</subject><subject>Space Sciences (including Extraterrestrial Physics</subject><subject>Spacecraft</subject><subject>Spacecraft propulsion</subject><subject>Trajectory optimization</subject><subject>Transportation</subject><subject>Transportation systems</subject><issn>0010-9525</issn><issn>1608-3075</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNp1kEtPwzAQhC0EEqXwA7hF4hxYx48kR1Txkir1AJwjx11TV20cbPcQfj0OAXFAnFa7882sNIRcUrimlPGbZwAKtSgELaEAYPyIzKiEKmdQimMyG-V81E_JWQhbAKhLJmdErfpo9_ZDReu6zJksbjCLXm1RR-eHn0volUbtlYmZ7QL6L9p20U3qECLuR3aDO-s0dtFbnTnf2hjOyYlRu4AX33NOXu_vXhaP-XL18LS4XeaaURnztWTARWvWuhIVas7qtipRC5H21hSInFfCJMXwCqRGToEJaQSVul4jbdmcXE25vXfvBwyx2bqD79LLpgDJZZm6KRJFJ0p7F4JH0_Te7pUfGgrN2GTzp8nkKSZPSGz3hv43-X_TJ-Xhdmw</recordid><startdate>20170501</startdate><enddate>20170501</enddate><creator>Konstantinov, M. 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The transition of the spacecraft from one orbit to another has been performed using an unpowered gravity assist maneuver near Venus and does not require the cruise propulsion operation. Each maneuver transfers the spacecraft into the sequence of operational heliocentric orbits. We have analyzed several systems of operational heliocentric orbits into which the spacecraft can be inserted by means of the considered transportation system with electric propulsion (EP). The mass of the spacecraft delivered to these systems of operational orbits has been estimated.</abstract><cop>Moscow</cop><pub>Pleiades Publishing</pub><doi>10.1134/S0010952517020034</doi><tpages>10</tpages></addata></record> |
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subjects | Astronomy Astrophysics and Astroparticles Astrophysics and Cosmology Electric propulsion Inclination Orbit insertion Orbits Physics Physics and Astronomy Polar environments Polar regions Solar orbits Space Exploration and Astronautics Space Sciences (including Extraterrestrial Physics Spacecraft Spacecraft propulsion Trajectory optimization Transportation Transportation systems |
title | Optimization of the trajectory of the spacecraft insertion into the system of heliocentric orbits |
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