Abstract
Hypergolic reactions may be useful in civil and military applications. In the area of rocket propulsion, they constitute a potential oeld due to the reduced Zeight and comple(ity of fuel inMection systems, alloZing yet controlled use of the propulsors. This manuscript aimed at presenting different hypergolic systems and their particularities, comparing them Zith chemical propulsion systems, Zhich are most commonly employed in rocket motors, for e(ample.
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