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Solid Propulsion Systems

Research has been made on a wide range of propulsion systems, including solid, ducted and hybrid rockets.
The characteristics of solid propellants, including ingredients, mechanical properties, burn rate, generated energy, andburning processes, are examined to design and develop high performance, high reliability rocket motors.
With various types of analyzers and optical observation apparatus, characteristics of explosives and organic/inorganic materials are also explored. The overall performance of a rocket motor is evaluated at our in-house test site for up to 200kN thrust level and at customer's test site for the full-size motor with more than 200kN of thrust.

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