Topic 2A.2 - Gravitation Flashcards

1
Q

What is gravitational field strength?

A

The force experienced per unit mass with a particle of small mass when placed at a point within the field.

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2
Q

What are the units of gravitational field strength?

A

Newtons per kilogram

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3
Q

What is Newton’s Universal Law of Gravitation?

A

Every particle in the universe attracts every other particle with a force that is directly proportional to the product of their masses, inversely proportional to the square of thr distance between them and acts on the line joining their centres.

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4
Q

Equation for gravitational attraction

A

F = Gmm/ d(squared)

Force = Gravitational constant x mass 1 x mass 2 / squared distance

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5
Q

In what direction is gravitational force?

A

Always attractive no matter the charge

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6
Q

What the units for the period of an orbit?

A

Seconds

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7
Q

Kepler’s 1st law

A

All planets move in an elliptical orbit with the sun at one foci

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8
Q

Kepler’s 2nd law

A

The radius vector drawn from the sun to the planet sweeps equal area in equal time intervals.

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9
Q

Kepler’s 3rd law

A

The period of revolution of a satellite is proportional to the radius of the orbit cubed

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10
Q
polar orbits
(4 key points)
A

pass over both the north and south poles
very small altitude over the Earth
gather very detailed images of the earth’s surface
orbit Earth 14.2 times per day

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11
Q

geostationary orbits

A

fixed over one place on the Earth’s surface
move in same direction as the earth with the same period of revolution
have an equatorial orbit
7 x radius of the Earth

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12
Q

Use of geostationary satellites

A

communication

internet

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13
Q

Use of polar satellites

A

weather???
surveillance
research

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14
Q

How to derive the gravitational field equation

g of planet

A
F = Gm1m2/d2
F = ma = mg

mg = Gm1m2/d2

g = Gm/d2

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15
Q

How to derive the velocity equation

A

For a satellite F (centripetal) = F (gravity)
Therefore,
mv2/r = Gm1m2/r2

v2=Gm/r
v = `|Gm/r

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16
Q

Why is the centre of the earth always the centre of a satellites orbit?

A
  1. satellites are moving with UCM
  2. UCM requires a force directed towards the centre of the circular path
  3. Gravity provides the force for the satellite
  4. Gravity is directed towards the centre of the Earth
  5. Therefore, the centre of the Earth coincides with the centre of the orbit
17
Q

Derive Kepler’s 3rd law

A
Fc = Fg
mv2/r = GMm/r2
v2 = GM/r
v = `|GM/r

v = 2 x pi x r/T
substitute v into equation and solve for T