Advanced Pulsed Plasma Thrusters and Their Application as a Part of Small Spacecraft Propulsion Systems
- 作者: Bogatyi A.V.1, El’nikov R.V.1, Nazarenko I.P.1, Popov G.A.1, Semenikhin S.A.1
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隶属关系:
- Moscow Aviation Institute (National Research University)
- 期: 卷 61, 编号 3 (2018)
- 页面: 445-451
- 栏目: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230635
- DOI: https://doi.org/10.3103/S1068799818030194
- ID: 230635
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详细
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.
作者简介
A. Bogatyi
Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: boga-alex@yandex.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
R. El’nikov
Moscow Aviation Institute (National Research University)
Email: boga-alex@yandex.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
I. Nazarenko
Moscow Aviation Institute (National Research University)
Email: boga-alex@yandex.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
G. Popov
Moscow Aviation Institute (National Research University)
Email: boga-alex@yandex.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
S. Semenikhin
Moscow Aviation Institute (National Research University)
Email: boga-alex@yandex.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
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