On 8/31/13 2:31 PM, Dan Riley wrote:
>
> 1204.2507 accounts for the deceleration via approximately equal
> contributions from differential emissivity of the RTGs and
> non-isotropic radiative cooling from the electronics in the main body
> of the spacecraft, which are covered in VIII C and VIII D
> respectively. (I'll also note that, while the RTG portion of the
> 1204.2507 model isn't as detailed as it is for the main body of the
> spacecraft, it is still considerably more developed than the arguments
> in 0104064).
I finally numerically duplicated the methodology in 1204.2507
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.
The astrophysical importance of this constant aP contribution
demands attention. 1204.2507 conclusions should be executed:
First,
Pioneer 11 data should be analyzed
Second,
the anomalous spin-down of both spacecraft
should be addressed considering the asymmetrically electrical (door) aP
would have very little influence on the Pioneer moment arm (M*R^2)
primarily represented by the 30 foot magnetometer boom.
The spin deceleration may be another indication of constant aP
linking Pioneer rotational angular momentum to translational momentum.
Third,
Analysis early trajectory data for indication of aP onset
comparable to a constant 5.9x10^-10 m/s^2
Fourth,
Address the possibility of outgassing
from surface materials, with potential observable contribution
to the anomalous acceleration.
Fifth,
Our understanding of systematics in the
Doppler tracking data can be improved
by a detailed auto correlation analysis.
Sixth,
Measure RTG paint emissivity by a thermal vacuum
chamber test of a hot RTG analogue.
(Resolve scenarios one and two)
Seventh,
Analyze other redundant data
in the form of Deep Space Network signal strength measurements,
which could be used to improve our understanding
of the spacecraft's precise orientation.
There is a lot of work to do.
The particle physicists at LHC would love this problem
considering the statistical ambiguity of their work
and the potential scientific importance of its outcome.
(something requiring no new physics)
I would love to analyze more detailed abundant available data.
No spacecraft of this type will be launched
within the foreseeable future.
I have had to digitize the reported data.
Surely the data is available in textual format
for the scientific community.
Richard D Saam