傳統且成熟的固推點火方式多以電控系統觸發，而點火系統可能會受到發動機空間配線的限制，或者點火器構造成火箭發動機重量增加，隨著奈米金屬材料獨特光熱轉換的興新研究，也許能以非介入式遠端閃光點燃啟動固態火箭，若是能藉由閃光點燃不但能減輕發動機重量、還能簡化整個系統。
本研究欲藉由奈米鋁粉閃光點燃的特性，混合硝化纖維與高氯酸銨(Ammonium perchlorate, AP)製作出一個高能的閃光點燃點火藥，本研究涵蓋從製程調配到點燃機制探討再到實際工程應用，其中以不同設備進行點火藥的特性分析再搭配不同的實驗的觀察，找出閃光點燃機制的反應過程。
最後以一具小型發動機驗證閃光點火系統，證實了此創新點火藥應用於非介入式遠端點燃固體火箭概念的可行性。

SUMMARY
In this study, we develop a novel and high energetic flash igniter which combines of nano-aluminum (nAl) powder and Nitrocellulose (NC) and Ammonium perchlorate (AP). The ignition mechanism of the flash igniter is deduced through the comparison between the Thermogravimetric Analysis(TGA) characteristic analysis and the experiments, and we also validate the feasibility of the flash ignition system with a small motor. We prove the feasibility of this novel nano Aluminum flash igniter can be applied to the concept of non-intervening ignited of solid rocket by this motor.

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