| 摘要 |
<p>The present invention relates to flares and other solid propellant devices, rockets or the like, equipped with an igniter or igniter system which is based in whole in part on an extruded igniter stick. The extruded igniter stick is formed from constituents comprising a water-soluble or water-swellable binder, at least one oxidizing agent, at least one fuel, and optionally, fibers.</p> |
