Advanced Pulsed Plasma Thrusters and Their Application as a Part of Small Spacecraft Propulsion Systems


如何引用文章

全文:

开放存取 开放存取
受限制的访问 ##reader.subscriptionAccessGranted##
受限制的访问 订阅存取

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

补充文件

附件文件
动作
1. JATS XML

版权所有 © Allerton Press, Inc., 2018