By and large, there are two types of the embodiment of these spacecraft module bodies for the below.
☆EXAMPLES OF PERFORMANCE OF THE INVENTION
FOR THE SUPER POWER DRIVING EQUIPMENT☆
The above movable shooting machines could be re-moved on glider flights in the atmosphere, just taking a center of gravity (i.e. balance between the right and the left and/or before and behind) of the whole body into consideration.
*Some vibration resistance devices should be securely placed in a connection part between the space propulsion module & the space plane (command module), if necessary.
[A trihedral figure of the main body (as a propulsion module of thespacecraft)] ~An abridged version of the eight (symmetrical) shooting machines~ The above design version may be chiefly applied to the following type(s) of the spacecraft Orion-like or....
*Some vibration resistance devices should be securely placed in a connection part between the space propulsion module & the space plane (command module), if necessary. [The Comparison with the existing Rocket Thrust etc]
As for performance of the above rocket engine (thrust),
its initial velocity is extremely greater than the other ones.
However, it has slowed down to get to the lunar surface
because of the influence of Earth gravity (which extends to infinity..)
in one time (or several times) only rocket fuel (combustion gas) injection.
On the contrary, in case of the super power drive performance
which can produce the driving forces many times
it will continue to accelerate more and more with ultra higher speed....