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Astronomy Principles and Practice Fourth Edition.pdf

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The astronomical unit 183<br />

For an exact balance, F G = F RP <strong>and</strong>, therefore,<br />

GM ⊙ ( 4 3 πa3 )ρ<br />

r 2 = L ⊙ πa 2<br />

4πr 2 c<br />

<strong>and</strong>, hence,<br />

a =<br />

L ⊙ 3<br />

GM ⊙ c 16πρ .<br />

Substituting for the various values <strong>and</strong> constants <strong>and</strong> by assuming a typical density of<br />

3000 kg m −3 , the balance of forces is achieved for a particle with radius<br />

3·8 × 10 26<br />

3<br />

a =<br />

6·67 × 10 −11 × 1·99 × 10 30 × 3 × 10 8 ≈ 0·2 µm.<br />

16π × 3 × 103 Thus, for such tiny dust particles emanating from a comet, no matter the distance from the Sun, they<br />

would continue to travel with their velocity at ejection <strong>and</strong> travel in a straight line without a force acting<br />

on them. Measurement of the movement of some parts of the cometary dust tail verifies this. The main<br />

body of the comet continues in its orbit about the Sun.<br />

There are proposals <strong>and</strong> design studies for utilizing radiation pressure as a means of propulsion<br />

within the solar system. By making very large ‘sails’ of light-weight material with high area-to-mass<br />

ratio, it is feasible to propel light-weight space vehicles using solar radiation as the ‘fuel’. By altering<br />

the attack of the sail at any time, the orbit of the vehicle can be readily modified at any time. The<br />

principles behind the manoeuvres are referred to as solar sailing.<br />

13.8 The astronomical unit<br />

In section 12.7 it was shown how an accurate scale model of the Solar System could be obtained, all<br />

the planetary distances being expressed in terms of the Earth’s distance from the Sun. Astronomers<br />

have found it convenient to use data connected with the Earth’s orbit <strong>and</strong> the Sun as their units of time,<br />

distance <strong>and</strong> mass. Newton’s precise statement of Kepler’s third law for a planet of mass m 2 revolving<br />

about the Sun of mass m 1 may be written in the form (see equation (13.31))<br />

k 2 (m 1 + m 2 )T 2 = 4π 2 a 3 .<br />

Taking the solar mass, the mean solar day <strong>and</strong> the Earth’s mean distance from the Sun as the units<br />

of mass, time <strong>and</strong> distance respectively, the equation becomes<br />

k 2 (1 + m 2 )T 2 = 4π 2 a 3<br />

where k 2 is written for G, the gravitational constant, <strong>and</strong> m 2 , T <strong>and</strong> a are all in the units defined earlier.<br />

The quantity k is called the Gaussian constant of gravitation.<br />

If, as was done by Gauss, the planet is taken to be the Earth <strong>and</strong> T given the value of 365·256 383 5<br />

mean solar days (the length of the sidereal day adopted by Gauss), while m 2 is taken to be 1/354 710<br />

solar masses, k is found to have the value 0·017 202 098 95, the value of a being, of course, unity. This<br />

distance, the semi-major axis of the Earth’s orbit, was called the astronomical unit (AU).<br />

The concept has since been refined. From time to time, various quantities have been determined<br />

more accurately but to avoid having to re-compute k <strong>and</strong> other related quantities every time,<br />

astronomers retain the original value of k as absolutely correct. This means that the Earth is treated like<br />

any other planet. The unit of time is now the ephemeris day. The Earth’s mean distance from the Sun is<br />

now taken as 1·000 000 03 astronomical units while the Earth–Moon system’s mass is 1/328 912 solar<br />

masses.

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