Comparative Design and Ballistic Analysis of Using Chemical and Electric Propulsion Systems in the Solar Probe Project

The possibility of implementing the solar probe project by launching a research satellite into the system of heliocentric orbits with a relatively small perihelion radius and a sufficiently large inclination to the solar equator (the inclination of the last heliocentric orbit to the plane of the sol...

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Veröffentlicht in:	Cosmic research 2019-09, Vol.57 (5), p.325-338
1. Verfasser:	Konstantinov, M. S.
Format:	Artikel
Sprache:	eng
Schlagworte:	Astronomy Astrophysics and Astroparticles Astrophysics and Cosmology Chemical propulsion Design analysis Electric propulsion Equator Inclination Launching Orbits Organic chemistry Physics Physics and Astronomy Propulsion systems Satellites Solar probes Space Exploration and Astronautics Space Sciences (including Extraterrestrial Physics Spacecraft Spacecraft propulsion Transportation systems
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