Test of B/Ti multilayer reactive igniters for a micro solid rocket array thruster

In this study, reactive B/Ti multilayer igniters were investigated for the noncontact ignition of a micro solid rocket array thruster in vacuum. When current is supplied to the B/Ti multilayer igniter, the chemical reaction: 2B + Ti → TiB 2 + 1320 cal/g occurs, and sparkles are spread to a distance...

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Veröffentlicht in:	Sensors and actuators. A. Physical. 2008-06, Vol.144 (2), p.361-366
Hauptverfasser:	Tanaka, Shuji, Kondo, Kazuyuki, Habu, Hiroto, Itoh, Akihito, Watanabe, Masashi, Hori, Keiichi, Esashi, Masayoshi
Format:	Artikel
Sprache:	eng
Schlagworte:	Igniter Microthruster Solid propellant
Online-Zugang:	Volltext
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