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Satellite Motion, Low Orbit, Short Period, Geosynchronous Orbit, Testing Models, Kepler’S Work, Kepler’S First Law, Orbital Speed, Kepler’S Second Law, Orbital Period are key points in this lecture. All important points and concepts related to physics are introduces and some explained in this course.
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-^ Use the force of universalgravitation.•^ Fgrav
= G M
m^ /^
(^2) r
^ The height for a satellite witha 24 hr period can be found.
(^22) 3
2 2
2
radius:
r^ = 4.22 x 10
7 m
altitude is
r^ - 6400 km = 36,000 km
(or
Ptolemaic
) means the Earth is at the
center and motionless. Heliocentric
(or
Copernican
) means the Sun is at the
center and motionless. Scholars wanted to differentiate models bycomparing the predictions with precise observations. This originated the modern
scientific method
.
A path connecting the two foci to theellipse always has the same length.
-^ GMm
(^2) / r =
(^2) mv / r
(^2) • v
/ r
^ Larger radius orbit means slower speed. ^ Within an ellipse larger distance also gives slowerspeed.
-^ Long – semimajor (
a )
-^ Short – semiminor (
b )
^ The area is
ab
(becomes
(^2) r for a circle).
^ The speed is related to theperiod in a circular orbit.
(^2) • v =^ GM
/ r
-^ (
r / T )
2 =^ GM
/ r (^2) • T = 4
23 r/GM
^ Larger radius orbit meanslonger period. ^ Within an ellipse, a largersemimajor axis also gives alonger period.
b a
23 / a
= constant
-^ The constant is the same for all objects orbiting the Sun
semimajor axis
:^ a
direction of orbitThe time for one orbitis one period:
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