Way 
1884. | 603 tChase, 
mg) and the mean eccentricity of the outer or subsident member are so 
influenced by the change of centripetal into tangential orbital motion 
that we find 
me” (1 + 65) Cindy ++ mg) = Ms. 
According to Stockwell, Neptune’s mean secular eccentricity, ¢, = 
.0100889. ILlence we derive the data for the following calculation : 
30.46955 1.4838661 
19. 183581 1.2829297 2 
1's) 1.1667527 0669788 
“1h 9942998 4 
1+ 6 - 0043381 5 
8.0208111 6 
(4+ 5 + 6) = log. 1 + (m, ++ m,) 4.0189490 7 
‘ N A 1.1667527 
log. (8) representing the ratio of mg :m,, log. mg = log. 3. 1667527 + (%, and 
1 
log. m, = log. 2.1667597 + 6)» 
2,1667527 3858093 8 
(7+ 8 =1+m, 4.3547583 9 
9 —3)=1+m, 4.2877795 10 
2. In the actions and reactions of the chief centres of nucleation (Sun), 
condensation (Earth), nebulosity (Jupiter), and planetary inertia (Saturn), 
the mass relation arises which is given in Note 445. 
1 -+ my = 829196 5.5174544 11 
1+ m,== 3501.6 3.5442665 12 
4 (11 + 12) 3.0205736 13 
3. In the Mars-Mercury belt, as modified by solar and terrestrial action 
(Note 489). 
a= 1.5236898 1828960 14 
A= 3870987 T.5878218 15 
(14 — 15) 5950742 16 
4 (16) 1.5789 1988581 17 
8098500 6.4904501 18 
(17 +- 18) 4884366 6. 6888081 19 
354986 5.5501499 20 
(18 + 11 —20) 2869151 6 4577546 21 
(19 + 11 —20) 4530150 6.6561126 22 
452. Change of Static to Rotary Hquilibrium. 
The following logarithms represent the influence of the change from 
static to rotary equilibrium as explained in Note 424. 
1 ++ a, = 1047.879 8.0208111 23 
p's 9391726 T.9727454 24. 
(28 — 24) 1115.747 3.04°75657 25 
(5 5.202798 7162869 26 
ps 214.4518 2,3318288 7 
rs 206264! 806247 58144251 Qs 
(28 — 27) % = 961/'.8254 2.9830963 29 
