Tuesday, February 18, 2014

Pioneer 11/10 and the Solar Mass

Pioneer 11/10 and the Solar Mass.
Even though the auto-called *scientific Community* accept, in a big proportion, that the Pioneer anomaly is related to its radioactive engine, there is another Satellite, the Ulysses orbiting the Sun, which show that the engine approach is absolutely erroneous. Ulysses has a positive acceleration when it is approaching the Sun and a negative one when it is moving away from it.

Ulysses orbiting the Sun. (Image from NASA, Hubble Satellite publication)

NASA, using the Assist Dynamics, provided de force to send the Pioneer outside the Solar System but it is the Sun who has the traveling absolute control after the NASA force stopped. Really Nature, as a whole, is what has the total control because the Satellite’s measured velocity depends on the equation used to find it. NASA is erroneously using the old static Newton Celestial Mechanics and the so called anomaly doesn’t exist because that Celestial Mechanics fail to calculate the real effect provoked by Nature.

The so called negative acceleration is only the difference between the values calculated with Newton equations and the Sun actual mass.  The force that provokes the Satellite acceleration is bigger than the calculated, since the actual mass is bigger than the used, which, of course, is also calculated with Newton gravitation equation.

Newton Equation    F = G M m / d2

Autodynamics Equation    F = G M* m* / d2  

F = Force,  G = Gravitational Constant,  M = Solar Mass,  m = Satellite mass, * = Mass Increment

The Autodynamics Celestial Mechanics provide a bigger value than the Newtonian one.

To see how the mass increment is get see:

A-20- Autodynamics Gravitation Applied to Lageos-Mercury.

To clear understand the Autodynamics Gravitation Mechanics see:

Quantum Universal Gravitation

Autodynamics is supported by many results get from many different applications

It explains: The motion creation (Planets Perihelion Advance and Lageos        

                    The increasing Gravitation in Eclipse Time.

                    The increasing Galaxies size looking at billions year far away.

                    Moon receding from Earth.

                    Spacecraft Assist micro-acceleration.

                    Gravitation Non-Propagation velocity. The Graviton has velocity;   Gravitation has NOT. It is actually present in the whole Universe.

It is Paramount to point it out here that the Autodynamics’ author didn’t invent neither any theory nor any particular hypothesis to explain each phenomenon.

It is a simple mechanism after elevating to a Universal Law two concepts very well known: Mass Decay-Energy Absorption.

We made a simple program to calculate the Solar mass correctly using the Pioneer 10-11 “real position and fly’s time”. (We are not totally sure of the data because NASA never answered any question).

From the program  output we include only three values for acceleration proving the given values and the actual Solar mass, which, of course doesn’t give any ***anomaly.*** The Pioneer position is given by Nature and the anomaly is introduce by ourselves, due to the fail of Newton Static equation corrected by Autodynamics , the New Paradigm by Carezani, as a dynamics one with his Quantum Universal Gravitation and consequently with his new Celestial Mechanics.

The Program.
#include <stdio.h>
#include <math.h>
#include <float.h>
#include <bios.h>

#define t 2.3974683E17     /* Seconds in 7.504 Billion/year */
#define d1 10.0E13            /* Pioneer d1 distance in cm */
#define d2 21.0E13            /*             d2                        */
#define d3 30.0E13            /*             d3                        */
#define G 6.67259E-8        /*  Gravitational Constant in cm^3/gr sec^2  */
#define M 1.9891E33         /* Sun Mass in gr */
#define P 2.6698913E30   /* All planets Mass in gr */
#define MP 1.99176989E33 /* Total Mass (Sun + Planets) in gr) */
#define Sy 3.157056E7        /* Second in ONE year */
#define a1c 10.3E-8             /* Anomaly Acceleration measure
#define a2c 8.05E-8             /*                                                     */
#define a3c 6.3E-8               /*                                                     */



          Double a1,a2,a3,as3,as1, a1t, a3t, ,M1,M2,M3,Minc,Msec,My,Mt,Mfo,A,


          Print(“         ***** NEWTON’S MECHANICS *****\n\n”);

          a1 = (G * M) / (d1 * d1);
          printf(a1 =%2.10E Acceleration at d1 distance\n\n”.a1);

          a2 = G * M) / (d2 * d2);
          printf (“a2 = %2.10E Acceleration at d2 distance\n\n”,a2);

          a3 = (G * M) / (d3 * d3);
          printf(“a3 = %2.10E Acceleration at d3 distance\n\n”,a3);

          printf(“            ***** CAREZANI’S MECHANICS*****\n\n”);
          M1 = (a1c * d1 * d1) / G;
          printf(“M1 = %2.15E Solar mass in time 1 \n\n”,M1);

          M2 = (a2c * d2 * d2) / G;
          printf(“M2 = %2.15E Solar mass in time 2 \n\n”,M2);

          M3 = (a3c * d3 * d3) / G;
          printf(“M3 = %2.15E Solar mass in time 3 \n\n”,M3);

          Msec = M / T;
          printf(“Msec = %2.10E Total mass increment per second\n\n”,Msec;

          My = Msec * Sy * 27;
          printf((“My = %2.10E Total mass increment in 27 year\n\n”,My);

          Mfo =  M + M3;
          printf(“Mfo = %2.15E Final observed mass (M+M3)\n\n”,Mfo);

          Mfc = M + My;
          printf(“Mfc = %2.20E Total (M+My) mass in 27 year\n\n\”,Mfc);

          Mi = (Mfo – Mfc) + M;
          printf(“Mi =2.29E Actual Sun Mass ((Mfo-Mfc)+M)\n\n”,Mi);

          Mad  = (Mi – M) / 1E33;
          printf(“Mad = %2.20E Mass ((Mi-M)/11E33) needed to be added to M\n\n”,Mad); 

           as3 =a3 +a3c;
          printf(“as3 =%2.15E Acceleration SUM (a3+a3c)\n\n”,as3);

          a3t = (G + Mi) / (d3 * d3);
          printf(“a3t = %2.15E Acceleration TEST ((G*Mi)/(d3*de)\n\n”,a3r);

          as1 = a1 +a1c;
          printf(“as1 = %2.15E Acceleration SUM (a1+a1C

          a1t = (G * Mi) / (d1 * d1);
           printf(“a1t = %2.15E Acceleration TEST((G*Mi)/(d1*d1)\n\n”,a1t);


          Program output: Only two values; Sum and Test

           as3 = 1.4747795298888E-3

           a3t =  1.4747795246456E-3

          as1 = 1.3272551769000E-2

          a1t = 1.32730157218106E-2

          Actual Sun Mass:

         1.989184967428E+033 A difference in the 5th decimal position.