The Sighter vehicle consists of a solid fuel motor 83mm in diameter and 1.4m in length to which ASRI has designed and attached various fins and nosecone modules. With a payload of 3kg, the Sighter has an apogee of 5.9km in about 40 seconds, experiencing a vicious 55g and 491m/s (Mach 1.4) during the flight.

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Launch Log

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ASRI Sighter with recovery module designed by University of Adelaide being prepared on rail and after at recovery location.

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