The AAMD was designed to address the concerns of deep space travel, in both the distance and time required. Today's rocket propulsion systems rely on expelling large amounts of fuel for short intervals and then coasting long intervals. This method is both expensive and time consuming where deep space is concerned.The AAMD is an alternative to rocket systems and it enables a vehicle to have a constant acceleration rates and deceleration rates. For instance, if the AAMD could provide a constant 1 G of acceleration and 1 G of deceleration, it would take less than a week to go from earth to mars, depending on their locations, whereas today's fastest rockets are 7 to 9 months, for the same trip.Slow and long travel times also are not good for the human body as the bones and muscle begin to deteriorate. The AAMD with its constant G applied to the occupants, will enjoy an artificial gravity produced by means of the constant acceleration. This would allow the occupants to have no breakdown in bones and muscle.The system uses of 2 counter rotating rotors and 8—orbital motors/generator per rotor, with—4 gyroscopes per orbital motor/generator. The moveable gyroscopes are capable of altering their location, from the main rotors axis. At the same time enable the other spinning mass to experience a balanced rotor the entire duration of the moveable weights altering their location of mass. The AAMD enables a means to impart linear movement in short increments of instantaneous directional linear thrust and follow the principle of the conservation of angular momentum.This is achieved and enables the vehicles propulsion system to have a 2 stage “push”-“pull” operation with controllable, directional thrust capability. If there was a need to move an object that is stationary, it is necessary to apply a force to influence it to do so. The AAMD can be powered by a nuclear reactor for extreme long range and ultra-high speeds to reach planets not feasible by means of rockets.


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    Title :

    Alternating Angular Momentum Drive-2 (AAMD)


    Contributors:

    Publication date :

    2025-01-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS




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