Advanced Pulsed Plasma Thrusters and Their Application as a Part of Small Spacecraft Propulsion Systems
The paper presents the research results of the effect of a capacitor energy storage device configuration on the specific characteristics of advanced modern propulsion systems based on the ablative pulsed plasma thrusters (APPT). These thrusters are designed to perform specific tasks within the small...
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| Veröffentlicht in: | Russian aeronautics 2018-07, Vol.61 (3), p.445-451 |
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| container_end_page | 451 |
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| container_issue | 3 |
| container_start_page | 445 |
| container_title | Russian aeronautics |
| container_volume | 61 |
| creator | Bogatyi, A. V. El’nikov, R. V. Nazarenko, I. P. Popov, G. A. Semenikhin, S. A. |
| description | The paper presents the research results of the effect of a capacitor energy storage device configuration on the specific characteristics of advanced modern propulsion systems based on the ablative pulsed plasma thrusters (APPT). These thrusters are designed to perform specific tasks within the small spacecrafts with the onboard power capacity up to 200 W. |
| doi_str_mv | 10.3103/S1068799818030194 |
| format | Article |
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| fulltext | fulltext |
| identifier | ISSN: 1068-7998 |
| ispartof | Russian aeronautics, 2018-07, Vol.61 (3), p.445-451 |
| issn | 1068-7998 1934-7901 |
| language | eng |
| recordid | cdi_proquest_journals_2160502392 |
| source | SpringerLink Journals - AutoHoldings |
| subjects | Ablation Aircraft and Rocket Engine Theory Automotive Engineering Energy storage Engineering Propulsion systems Pulsed plasma thrusters Spacecraft propulsion |
| title | Advanced Pulsed Plasma Thrusters and Their Application as a Part of Small Spacecraft Propulsion Systems |
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