Hybrid rocket motors offer potential for reducing the cost and weight of propulsion systems. Higher efficiency, and higher regression rate solid fuels can be leveraged into revolutionary system performance for a variety of missions from mars sample return to upper stage and micro-satellite propulsion.
Commercial applications are rapidly increasing with a reduction in the cost of access to space. N2O self-pressurizing Hybrid motors are viable low cost alternatives, as evidenced by their selection and use in spaceship one.
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