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rdsaam

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  1. I numerically duplicated (digitized) the methodology in Turyshev report 1204.2507
    It is concluded with RMS analysis,
    that Pioneer deceleration decays to a constant deceleration rather than zero
    analogous of an object passing through a fluid decelerating with Stokes' law.

    Aa. time (years after launch)(after AU to time conversion)
    Bb. electric contribution to aPelecx10^-10 m/s^2
    n = .406 half life 24.5 years regressing Table 1, 1204.2507
    aPelec = 7.75E-10*EXP(-LN(2)*time/24.5)
    Cc. RTG contribution to aPrtgx10^-10 m/s^2
    n = 0.0104 half life 87.72 years (Plutonium)
    aPrtg = 3.71E-10*EXP(-LN(2)*time/87.72)
    Dd. or Bb + Cc Total contribution to aPx10^-10 m/s^2
    Ee. Doppler measured aPx10^-10 m/s^2

    Scenario one
    Aa Bb Cc Dd Ee
    8.79 6.05 3.46 9.51 9.82
    10.78 5.71 3.41 9.12 9.33
    12.79 5.40 3.35 8.75 8.78
    14.82 5.10 3.30 8.40 8.21
    16.81 4.82 3.25 8.07 8.21
    18.80 4.56 3.20 7.75 7.39
    20.81 4.30 3.15 7.45 7.34
    22.82 4.07 3.10 7.17 7.23
    24.85 3.84 3.05 6.89 7.72
    Dd-Ee has RMS = .34

    ***************************************
    Statistical analysis of fin root temperatures
    http://arxiv.org/abs/gr-qc/0512121 Figure 20
    indicate temperature(T) half life of 130 years
    This translates into power half life ~emissivity*T^4
    or 130/4 or 32.5 years. This is not reflected
    in reported RTG power performance.
    Radiation flux during Pioneer 18 Jupiter flyby
    (10,000 times that of Earth)
    did not cause differential RTG emissivity.
    http://arxiv.org/abs/gr-qc/0104064 C
    does not provide any further mechanistic origin of Cc
    and none presented in 1204.2507
    Assuming RTG contribution(Cc) is replaced by
    a constant(Ff) the electric(Bb) + constant(Ff) or Gg
    yields RMS = .33 (equal to scenario one .34)
    when compared to doppler(Ee)

    Scenario two
    Aa Bb Ff Gg Ee
    8.79 6.05 3.33 9.38 9.82
    10.78 5.71 3.33 9.04 9.33
    12.79 5.40 3.33 8.73 8.78
    14.82 5.10 3.33 8.43 8.21
    16.81 4.82 3.33 8.15 8.21
    18.80 4.56 3.33 7.89 7.39
    20.81 4.30 3.33 7.63 7.34
    22.82 4.07 3.33 7.40 7.23
    24.85 3.84 3.33 7.17 7.72
    Gg-Ee has RMS = .33

    ***************************************
    A more detailed model Hh
    minimizing RMS at .27
    (the best available fit)
    assumes aP approaching a constant 5.9
    aP = (12.587-5.9)*EXP(-.068*time)+5.9

    Scenario three
    Aa Hh Ee
    8.79 9.60 9.82
    10.78 9.14 9.33
    12.79 8.74 8.78
    14.82 8.39 8.21
    16.81 8.09 8.21
    18.80 7.83 7.39
    20.81 7.60 7.34
    22.82 7.40 7.23
    24.85 7.23 7.72
    Hh-Ee has RMS = .27

    There is statistical logic
    within the context of 1204.2507 and historical Pioneer reports
    for a constant aP contribution.

    Richard D. Saam

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