Universal Gravitation Module
A. Defined: of between any two objects in the universe.
$G = 6.67 \times 10^{-11} \text{ Nm}^2/\text{kg}^2$
$m_1, m_2 = \text{masses attracting each other}$ | $r = \text{distance between centers}$
1. Relationship between Force ($F$) and distance ($r$): . Plot shape: .
2. Tripling the distance causes the Force to change by: .
3. Relationship between Force ($F$) and mass ($m$): . Plot shape: .
Ex 1) Two objects a distance $r$ apart have force $F$. Masses changed to $2m_1$ and $2m_2$, and distance changed to $4r$. New force?
Ex 2) If the gravitational force on satellite A is 160,000 N, what is the force on satellite B (same mass, double distance from center)?

Ex 3) A rocket weighs 18,000 N at surface. If it rises to a height where its distance from the center is 3 Earth radii, its weight is...

Earth Gravity Data: NY (9.803 m/s²) / Denver (9.796 m/s²) / North Pole (9.832 m/s²)
What explains these differences?
Formula for surface gravity: $g = \frac{G M_p}{r^2}$.
Ex 4) Mars mass is 1/10 Earth, diameter is 1/2 Earth. $g_{Mars} \approx $ .
28. A 2100-kg spacecraft is in orbit 2.0 Earth radii from the Earth's center. Calculate the force of gravity on the spacecraft.

32. A hypothetical planet has a radius 1.5 times that of Earth, but has the same mass. What is the acceleration due to gravity on its surface?

Ex 5) Prove orbital velocity is independent of satellite mass using the derivation above.
a) Orbital $v$ and Period $T$ are determined only by: .
b) The smaller the radius, the the orbital velocity and the period $T$.
1:C, 2:D, 3:B, 4:B, 5:D, 6:C, 7:B, 8:B, 9:A, 10:B, 11:A, 12:B, 13:D, 14:C, 15:C, 16:A, 17:B, 18:C, 19:C, 20:A, 21:B, 22:C, 23:B, 24:A, 25:B, 26:C, 27:D, 28:D, 29:A, 30:B, 31:A, 32:C, 33:B, 34:C, 35:C, 36:B, 37:D
During a lunar eclipse, the Moon ($m=7.4 \times 10^{22}$ kg, $r=3.8 \times 10^8$ m) and Sun ($m=2.0 \times 10^{30}$ kg, $r=1.5 \times 10^{11}$ m) are on opposite sides of the Earth ($m=6.0 \times 10^{24}$ kg).
A solid brass ball has a mass of 2.10 kilograms. The Moon has a radius of $1.74 \times 10^6$ meters and a mass of $7.35 \times 10^{22}$ kilograms.
A satellite of mass $m$ is in a circular orbit around the Earth (mass $M_e$) at a radius $a$ from the center of the Earth.