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9.2 Space: 3. The Solar System is held together by gravity

Syllabus reference (October 2002 version)
3. The Solar System is held together by gravity
Students learn to: Students:

Extract from Physics Stage 6 Syllabus (Amended October 2002). © Board of Studies, NSW.

Prior Learning: Preliminary module 8.5 (subsections 5 and 6)

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present information and use available evidence to discuss the factors affecting the strength of the gravitational force

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describe a gravitational field in the region surrounding a massive object in terms of its effects on other masses in it

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define Newton's Law of Universal Gravitation

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solve problems and analyse information using Newton's Law of Universal Gravitation equation

Sample problem

A geostationary satellite of mass 600 kg orbits at a distance of 35 800 km. Calculate the force of gravity that keeps the satellite in orbit.

Data: G = 6.67 x 10-11 N m2 kg-2

m1 = mass of Earth = 6.0 x 1024 kg

m2 = mass of satellite = 6.0 x 102 kg

d = 3.58 x 104 km = 3.58 x 107 m

F = G m1 m2 / d2

   = (6.67 x 10-11)( 6.0 x 1024)( 6.0 x 102) / (3.58 x 107)2

   = 187 N

Sample analysis

Describe the way in which gravitational force varies with distance for any two objects.

For any two objects chosen, for example, Earth and a Space Shuttle, the two masses m1 and m2 remain constant. G is also constant, therefore the equation can be reduced to:

F = k / d2

where k is a constant.

Therefore gravitational force is inversely proportional to the distance between the objects. Force diminishes very rapidly with distance at first, but diminishes more and more slowly as distance increases.

graph y=
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discuss the importance of Newton's Law of Universal Gravitation in understanding and calculating the motion of satellites

Background

Gravitation provides the centripetal force that produces the circular motion that is the satellite’s orbit around a planet. Therefore, it can be said that:

Gravitational force = Centripetal force

Gravitational force = Centripetal force equation

This equation shows that the required orbital velocity of a satellite depends upon the mass and the orbital radius. Note: this equation is NOT stipulated by the syllabus.

  • The following expressions can be derived, from the relationships described in the two lots of background information above:
    mathematical expressions

  • The second equation describes the relationship between the radius of an orbit and the period for any (and all) satellites, natural and artificial, orbiting the earth. This second equation is stipulated in the syllabus. It is also a more useful version of Kepler’s third law.
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identify that a slingshot effect can be provided by planets for space probes

Extra information outside the syllabus:

  • The manoeuvre can be analysed as an elastic collision, even though no actual contact occurs. A slingshot manoeuvre can therefore be used to change the spaceship's trajectory and velocity relative to the Sun, though the spacecraft's speed relative to the planet on effectively entering and leaving it's gravitational field, will remain the same-as it must according to the law of conservation of energy.

  • To a first approximation, from a large distance, the spacecraft appears to have bounced off the planet. The planet will have slowed very marginally, losing an equivalent amount of kinetic energy. (Recall that Ek = ½mv2 and the mass of a planet is very large so that the change in velocity of the planet will be very small.)
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