The C17 rocket motor uses fast burning non-aluminized HTPB/AP composite propellant (Hazard Class 1.3) to achieve a nominal total impulse of 1905 lbf-sec. ...+View More
C15/HEPI rocket motor
The C15/HEPI rocket motor uses non-aluminized HTPB/AP composite propellant (Hazard Class 1.8) ...+View More
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The Langkawi International Maritime and Aerospace Exhibition (LIMA Langkawi 2019)
