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Physics
Physics
Problem
A
1.0
×
10
3
kg
1.0\times10^{3}\,\text{kg}
1.0
×
1
0
3
kg
satellite orbits Earth in a circular path
3.0
km
3.0\,\text{km}
3.0
km
above Earth’s surface. Given
R
E
=
6.4
×
10
6
m
R_E = 6.4\times10^{6}\,\text{m}
R
E
=
6.4
×
1
0
6
m
,
M
E
=
6.0
×
10
24
kg
M_E = 6.0\times10^{24}\,\text{kg}
M
E
=
6.0
×
1
0
24
kg
, and
G
=
6.67
×
10
−
11
N
m
2
kg
−
2
G = 6.67\times10^{-11}\,\text{N}\,\text{m}^2\,\text{kg}^{-2}
G
=
6.67
×
1
0
−
11
N
m
2
kg
−
2
, determine the satellite’s kinetic energy. a)
4.3
×
10
10
J
4.3 \times 10^{10}\,\text{J}
4.3
×
1
0
10
J
b)
3.1
×
10
10
J
3.1 \times 10^{10}\,\text{J}
3.1
×
1
0
10
J
c)
2.1
×
10
10
J
2.1 \times 10^{10}\,\text{J}
2.1
×
1
0
10
J
d)
1.5
×
10
10
J
1.5 \times 10^{10}\,\text{J}
1.5
×
1
0
10
J
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