ADN-BASED PROPULSION FOR SPACECRAFT -KEY REQUIREMENTS AND EXPERIMENTAL VERIFICATION
ADN-BASED PROPULSION FOR SPACECRAFT -KEY REQUIREMENTS AND EXPERIMENTAL VERIFICATION
复制标题
DOI：
10.2514/6.2004-4145
复制
发表时间：
2004-07
期刊：
影响因子：
--
通讯作者：
Tor-Arne Grönland;K. Anflo;G. Bergman;R. Nedar
中科院分区：
文献类型：
--
作者：
Tor-Arne Grönland;K. Anflo;G. Bergman;R. Nedar
本文介绍了一种基于氨酰胺、ADN及相关火箭发动机技术的航天器推进用可储存液体单推进剂的研制工作。与单一推进剂联氨相比，这项工作的主要目标是减少操作危险并提高性能。先前的论文1,2,3,4描述了ADN的基本特性，可能的推进剂成分和小型火箭发动机试验发射的实验结果。
This paper describes the ongoing work to develop a storable liquid monopropellant for spacecraft propulsion based on Ammoniumdinitramide, ADN, and related rocket engine technologies. The primary objective of this effort is to reduce operational hazards and improve performance as compared with monopropellant hydrazine. Previous papers 1,2,3,4 have described the basic properties of ADN, possible propellant compositions and experimental results from test firings of small rocket engines.