Geocentric Latitude |
Cell length |
Torque |
Equivalent to torque energy |
---|---|---|---|
0 | Sarcoma cell | 9.107×10-10 | 0.09107 fJ |
30 | 9.126×10-10 | 0.09126 fJ | |
45 | 50 | 9.145×10-10 | 0.09145 fJ |
60 | 9.164×10-10 | 0.09164 fJ | |
90 | 9.183×10-10 | 0.09183 fJ | |
Human Egg | Nace’s result 1.5x10-8 | dyne cm | |
0 | 1.118×10-8 | 1.200 fJ | |
30 | 89 | 1.120×10-8 | 1.120 fJ |
45 | 1.123×10-8 | 1.123 fJ | |
60 | 1.125×10-8 | 1.125 fJ | |
90 | 1.128×10-8 | 1.128 fJ | |
Nace’s result 0.85 dyne cm | |||
0 | 0.818 | 81.860 nJ | |
30 | 31000 | 0.820 | 82.031 nJ |
45 | 0.822 | 82.204nJ | |
60 | 0.824 | 82.380 nJ | |
90 | 0.825 | 82.550 nJ |
Orbital Eccentricity |
Cell length |
Torque |
Equivalent Energy |
---|---|---|---|
Sarcoma cell | 9.045×10-10 | 0.0904 fJ | |
9.067×10-10 | 0.0906 fJ | ||
50 | 9.089×10-10 | 0.0908 fJ | |
Human Egg | 1.110×10-8 | 1.110 fJ | |
1.113 × 10-8 | 1.113 fJ | ||
89 | 1.116× 10-8 | 1.116 fJ | |
0.800 | 80.00 nJ | ||
0.803 | 80.30 nJ | ||
31000 | 0.804 | 80.40 nJ |
orbital semimajor axis. | |
eccentricity of the orbit. | |
argument of latitude. | |
true anomaly. | |
constant of universal gravitation. | |
orbital inclination. | |
radial orbital distance of the spacecraft from the center of the Earth. | |
oblateness coefficient of the Earth. | |
the mass of the Earth. | |
mass of any planet. | |
total gravitational potential of the Earth. | |
define a right handed coordinate system. | |
applied force. | |
distance of the center of mass that the force is applied to the axis of rotation. | |
distance between the centers of the heavy and light masses in the cell. | |
total cell length. | |
where, where |
|
the radius of the cell. | |
density of the medium. | |
density of the heavy mass. | |
density of light mass. | |
constants in the range [0,1]. | |
corrected gravitational acceleration. | |
torque. | |
radius of the Earth. | |
equatorial radius of the Earth. | |
polar radius of the Earth. | |
flattening of the Earth. | |
flattening of Mars. | |
planetary flattening. | |
orbital mean anomaly. | |
spacecraft mean angular velocity. | |
geocentric latitude. | |
angular velocity of the Earth. | |
colatitude. | |
argument of the perigee. | |
argument of the ascending node. | |
geocentric longitude. | |
is the angle between |
|
mean longitude. |
Orbital Eccentricity |
Cell length |
Torque |
Equivalent Energy to torque |
---|---|---|---|
Sarcoma cell | 8.340×10-10 | 0.0834 fJ | |
8.360×10-10 | 0.0836 fJ | ||
50 | 8.376×10-10 | 0.8376 fJ | |
Human Egg | 1.024×10-8 | 1.024 fJ | |
1.026×10-8 | 1.026 fJ | ||
89 | 1.028×10-8 | 1.028 fJ | |
0.750 | 75.000 nJ | ||
0.751 | 75.100 fJ | ||
31000 | 0.752 | 75.200 fJ |
Orbital Eccentricity |
Cell length |
Torque |
Equivalent Energy to torque |
---|---|---|---|
Sarcoma cell | 8.340×10-10 | 0.0834 fJ | |
8.356×10-10 | 0.0835 fJ | ||
50 | 8.375×10-10 | 0.0837 fJ | |
Human Egg | 1.024×10-8 | 1.024 fJ | |
1.026×10-8 | 1.026 fJ | ||
89 | 1.028×10-8 | 1.028 fJ | |
0.750 | 75.000 nJ | ||
0.751 | 75.100 nJ | ||
31000 | 0.753 | 75.300 nJ |
Orbital Eccentricity |
Cell length |
Torque |
Equivalent Energy |
---|---|---|---|
Sarcoma cell | 1.1809×10-9 | 0.1180 fJ | |
1.1846×10-9 | 0.1184 fJ | ||
50 | 1.1883 × 10-9 | 0.1188 fJ | |
Human Egg | 1.4499×10-8 | 1.4499 fJ | |
1.4546×10-8 | 1.4546 fJ | ||
89 | 1.4591×10-8 | 1.4591 fJ | |
1.0615 | 106.150 nJ | ||
1.0648 | 106.480 nJ | ||
31000 | 1.0681 | 106.810 nJ |