GK2 Propulsion System

A. Steinbeck, J. Chae, M. Abele
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引用次数: 0

Abstract

This paper describes briefly the Chemical Propulsion System (PS) which has been used in the Korean bi-propellant Geostationary Satellite. The new commonly developed platform (GK2) went after design through acceptance test and final check out at launch site in Kourou. All this steps has been performed in a very close partnership between Korean Aerospace Research Institute (KARI) and ArianeGroup. In addition the common working approach between the Korean Aerospace Research Institute and the private company ArianeGroup GmbH will be illustrated which has been let to a successful partnership in development of a new propulsion platform - successfully flown first time December 2018. Besides this technical topic this partnership developed the dimension of a certain kind of Koreanisation in the field of bi-propellant space propulsion.
GK2推进系统
本文简要介绍了韩国双推进剂地球同步卫星所采用的化学推进系统(PS)。新的共同开发的平台(GK2)经过设计,通过验收测试和在Kourou发射场的最终检查。所有这些步骤都是在韩国航空航天研究所(KARI)和阿丽亚娜集团之间非常密切的伙伴关系下执行的。此外,还将说明韩国航空航天研究所与私营公司阿丽亚娜集团有限公司之间的共同工作方法,该方法已成功合作开发了一种新的推进平台,并于2018年12月首次成功飞行。除了这个技术问题外,这种伙伴关系还在双推进剂空间推进领域发展了某种朝鲜化的维度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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