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ASTRONOMY 205.1 GENERAL ASTRONOMY I
“Solutions” Sheet
Student Name
Laboratory Exercise 8. The Orbit of the Earth about the Sun
Purpose. To infer a basic knowledge of the Earth’s orbit about the Sun from simple observations.
Procedure. See Laboratory Manual.
Equipment.



images of the Sun taken near perihelion and aphelion
millimetre ruler
spectra of Arcturus taken at times of maximum and minimum approach speeds
Data.
1. Orbital Eccentricity.
Aphelion Image (at left above)
Orientation
Position 0°
Measured Diameter, Da
(millimetres)
Perihelion Image (at right above)
Orientation
Position 0°
Measured Diameter, Dp
(millimetres)
Average aphelion diameter, Da
Position 45°
Position 90°
Position 135°
Position 45°
Position 90°
Position 135°
=
millimetres ±
millimetres
Average perihelion diameter, Dp
Dp  Da
Orbital eccentricity, e =
Uncertainty, e = 2 Dp
=

Dp  Da
D  D 
D  D 
p
p
millimetres ±
a
2
millimetres
=

=
a
Computed orbital eccentricity = eexp ±eexp
=
±
Accepted value of e = 0.0167.
Comparison of Values and Comments.
2. Earth’s Orbital Speed.
Measured Positions of Iron Arc Emission Lines
Line
1
2
3
Wavelength 4260.48 Å 4271.16 Å 4271.76 Å
Position
(millimetres)
4
4282.41 Å
5
4294.13 Å
6
4299.24 Å
7
4307.91 Å
Scale of spectrogram (in Å/mm) from attached graph† =
(† Make the graph yourself and append it to the lab writeup.)
Measured Positions of Stellar Iron Arc Absorption Lines
Spectrum a. Recession.
Line
1
2
3
4
Wavelength 4260.48 Å 4271.16 Å 4271.76 Å 4282.41 Å
Offset
(millimetres)
Spectrum b. Approach.
Line
1
Wavelength 4260.48 Å
Offset
(millimetres)
Spectrum a. Recession.
Line
1
Wavelength 4260.48 Å
Offset
(Å)
Spectrum b. Approach.
Line
1
Wavelength 4260.48 Å
Offset
(Å)
Spectrum b. Approach.
Line
1
Wavelength 4260.48 Å
Velocity
(km/s)
6
4299.24 Å
7
4307.91 Å
2
4271.16 Å
3
4271.76 Å
4
4282.41 Å
5
4294.13 Å
6
4299.24 Å
7
4307.91 Å
2
4271.16 Å
3
4271.76 Å
4
4282.41 Å
5
4294.13 Å
6
4299.24 Å
7
4307.91 Å
2
4271.16 Å
3
4271.76 Å
4
4282.41 Å
5
4294.13 Å
6
4299.24 Å
7
4307.91 Å
Line Velocities Calculated using v
Spectrum a. Recession.
Line
1
Wavelength 4260.48 Å
Velocity
(km/s)
5
4294.13 Å

observed  rest
λrest
 2.99792458  10 5 km s -1
2
4271.16 Å
3
4271.76 Å
4
4282.41 Å
5
4294.13 Å
6
4299.24 Å
7
4307.91 Å
2
4271.16 Å
3
4271.76 Å
4
4282.41 Å
5
4294.13 Å
6
4299.24 Å
7
4307.91 Å
Average velocity of recession, vA
=
km/s ±
km/s
Average velocity of approach, vB
=
km/s ±
km/s
Earth’s orbital speed, vE =
1
2
vA  vB 
0.85896

1
2
vA  vB  =
0.85896
±
km/s
Star’s space velocity, v* =
1
2
vA  vB 
0.85896

1
2
vA  vB 
=
±
0.85896
Accepted value of vE = 29.786 km/s.
Accepted value of v* = –5 km/s.
Comparison of Values and Comments.
3. The Astronomical Unit.
R 
Experimental Value of A. U.,
vE P vE  365.256363  86400 s/day

2
2  3.14159

km
R 
Experimental Uncertainty, A. U.,
vE P vE  365.256363  86400 s/day

2
2  3.14159

Accepted value of 1 A.U. = 1.495978707 × 108 km
Comparison of Values and Comments.
Discussion.
Conclusions.
km
km/s
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