The Gravitational Spacecraft

d d Gravitational Spacecraft The total gravitational mass of the spacecraft, M gS total , can be expressed by means of the following expression: M gS total  M gS  2 M gP , where M gS is the total gravitational mass of the spacecraft without the gravitational mass, 2 M gP , of the two tungsten plates (in blue) . Assuming that the density of external electromagnetic energy in M gS is negligible, then we can write that M gS  M i 0 S , where M i 0 S is the rest inertial mass of the spacecraft (without the two tungsten plates). On the other hand, since 4 14   M gP  M i 0 P   1  2 1  6.70  10 V d   1 M i 0 P , we can write that    4 14   M gS total  M gS  2M gP  M i 0 S  2 1  2 1  6.70 10 V d   1 M i 0 P    For example, if M i 0 S  10,000kg ; M i 0 P  10kg ; V  1558.54volts and d  0.05m , then equation above yields M gS total  10,000  999.99 10  0.1kg . This means that, on the Earth surface, the weight of the spacecraft becomes less than 1N !!! Mach’s principle predicts that inertial forces acting on a particle are the result from the gravitational interaction between the particle and the other particles of the Universe. Thus, the inertial forces Fii acting on a particle are proportional to gravitational mass, m g , of the particle, i.e., Fii  mg ai [1]. This fact shows that the inertial effects upon a spacecraft can be strongly reduced because, as it shown above, the gravitational mass of the spacecraft M gS total can be strongly reduced ( Fii  M gS total a i ). In practice, it means that will be possible to become quasi-null the inertial properties of the spacecraft. Under these circumstances, the spacecraft can describe incredible trajectories, and to make super accelerations and super decelerations in a very short time interval (<1s), without be destructed. [1] De Aquino, F. (2010) Mathematical Foundations of the Relativistic Theory of Quantum Gravity, Pacific Journal of Science and Technology,11 (1), pp. 173-232. Available at https://hal.archives-ouvertes.fr/hal- 01128520