Plasma Accelerator Utilizing the Medium of Near-Earth Space for Orbital Transfer Vehicles

Author:

Karimov Alexander R.12ORCID,Murad Paul A.3,Yamschikov Vladimir A.4,Baranov Dmitriy S.2

Affiliation:

1. Institute for Laser and Plasma Technologies, National Research Nuclear University MEPhI, Kashirskoye Shosse 31, Moscow 115409, Russia

2. Institute for High Temperatures, Russian Academy of Sciences, Izhorskaya 13/19, Moscow 127412, Russia

3. Kepler Aerospace Ltd., 2908 Enterprise LN, Midland, TX 79706, USA

4. Institute for Electrophysics and Electric Power, Russian Academy of Sciences, Dvortsovaya Naberezhnaya, 18, St. Petersburg 191186, Russia

Abstract

The development of plasma accelerators for spacecraft propulsion that can capture space matter and energy shows great promise for spacecraft advancement. Such a technical approach offers a viable solution to the challenges associated with traditional rocket fuel. In the present paper, we explore the utilization of interplanetary matter as fuel for plasma thrusters on space vehicles, specifically for flights within the vicinity of Earth. Herein, solar radiation is considered a source of energy for the ionization and acceleration of particles captured from the space environment.

Funder

Ministry of Science and Higher Education of the Russian Federation

Publisher

MDPI AG

Subject

Fluid Flow and Transfer Processes,Computer Science Applications,Process Chemistry and Technology,General Engineering,Instrumentation,General Materials Science

Reference47 articles.

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2. Ulrich, W. (2012). Astronautics: The Physics of Space Flight, Wiley& Sons. [2nd ed.].

3. Goebel, D.M., and Katz, I. (2008). Fundamentals of Electric Propulsion: Ion and Hall Thrusters, Wiley.

4. Electrodeless plasma thruster for spacecraft: A review;Bathgate;Plasma Sci. Technol.,2017

5. Fundamentals of stationary plasma thruster theory;Kadomtsev;Reviews of Plasma Physics,2000

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