Systems, methods, and apparatus for providing a multi-fuel hybrid rocket motor

An apparatus comprising:

• a rocket comprising:
• a multi-fuel rocket motor comprising:
• a body comprising:
• an interior surface and an exterior surface;
• an intake port;
• and
• an exit nozzle;
• a channel connecting the intake port with the exit nozzle, the channel comprising a longitudinal axis;
• a turbulator fin extending from the interior surface and into the channel connecting the intake port with the exit nozzle, wherein the turbulator fin extends in a helicoidal pattern along the longitudinal axis of the channel;
• at least one cavity, wherein the cavity is defined based at least in part on the turbulator fin and wherein the at least one cavity is in fluid communication with the channel;
• and
• a propellant fuel disposed within the at least one cavity, wherein at least a portion of the propellant fuel is exposed to the channel and wherein the propellant fuel has a higher burn consumption rate than the turbulator fin.

A method for producing a multi-fuel rocket motor, the method comprising:

• forming a motor casing body comprising:
• an interior surface and an exterior surface;
• an intake port;
• and
• an exit nozzle;
• forming a channel connecting the intake port with the exit nozzle, wherein the channel comprises a longitudinal axis;
• forming a plurality of turbulator fins within the motor casing body, each of the plurality of turbulator fins extending from the interior surface of the motor casing body and into the channel, wherein each of the plurality of turbulator fins extends in a helicoidal pattern along a longitudinal axis of the at least one channel;
• and
• at least one cavity defined by the plurality of turbulator fins and in fluid communication with the channel;
• and
• depositing a propellant fuel within the at least one cavity, wherein at least a portion of the propellant fuel is exposed to the channel and wherein the propellant fuel has a higher burn consumption rate than the plurality of turbulator fins.