Computer Science – Performance
Scientific paper
Oct 2004
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004esasp.557e..28c&link_type=abstract
Proceedings of the 2nd International Conference on Green Propellants for Space Propulsion (ESA SP-557). 7-8 June 2004, Chia Lagu
Computer Science
Performance
Scientific paper
Hypergolicity is a very important characteristic for bipropellants. With hypergolic propellant, the design of engines and the handling of rocket systems are greatly simplified, and the rocket engine can be restarted repeatedly for a great number of times. Hydrogen peroxide and kerosene have been proposed as one of the best potential alternatives for replacing the toxic nitrogen tetroxide and unsymmetrical dimethyl hydrazine bipropellants currently in use. In this paper, composite hypergolic bipropellants have been developed by using high concentration hydrogen peroxide as the oxidizer for kerosene based fuels. The ignition-delay properties as well as the storage stability were extensively examined. Reliable ignitions and stable combustion performances were exhibited for over 500 times of cold start firing tests. In addition, satisfactory properties close to that of the traditional toxic hypergolic propellants have been observed in a 5 ton grade thruster.
Chen Wei
Cong Yang
Dou H.
Liang Dengfeng
Lin Gang
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