Advanced Pulsed Plasma Thrusters and Their Application as a Part of Small Spacecraft Propulsion Systems
- Авторлар: Bogatyi A.1, El’nikov R.1, Nazarenko I.1, Popov G.1, Semenikhin S.1
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Мекемелер:
- Moscow Aviation Institute (National Research University)
- Шығарылым: Том 61, № 3 (2018)
- Беттер: 445-451
- Бөлім: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230635
- DOI: https://doi.org/10.3103/S1068799818030194
- ID: 230635
Дәйексөз келтіру
Аннотация
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.
Авторлар туралы
A. Bogatyi
Moscow Aviation Institute (National Research University)
Хат алмасуға жауапты Автор.
Email: boga-alex@yandex.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
R. El’nikov
Moscow Aviation Institute (National Research University)
Email: boga-alex@yandex.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
I. Nazarenko
Moscow Aviation Institute (National Research University)
Email: boga-alex@yandex.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
G. Popov
Moscow Aviation Institute (National Research University)
Email: boga-alex@yandex.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
S. Semenikhin
Moscow Aviation Institute (National Research University)
Email: boga-alex@yandex.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993