Elements of United Physics for Aerospace Propulsion, Radiative Medium Motion and Intellect Background with Experimental Confirmation

Aerospace thermo physical problems and propulsion experience are analyzed in the light of modern experimental achievements of applied physics and astrophysics. The analysis demonstrates ? need to move from the modern double standard physics (nonlinear standard and its linearized quantum-relativistic variants) to united standard of the classic physics for aerospace propulsion design. For the common classic physics design standard the thermodynamically compatible conservation laws of mass, momentum and energy for radiate gaseous medium are written at presence of the external cosmic thermostat with the temperature 2.73 K. By that the entropy growth presents the dissipative energy value on the level of this cosmic thermostat gives pressure losses and determines the one time arrow. Some aspects of recording and storage of intellect information are also considered. The paper contains typical examples for aerospace propulsion solutions and simulation cosmic jets and waves.