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   Home  Educational  Meteors  Earth Cross Section for Meteoroids Sunday, Oct 12 2008 10:51 UT
Space Debris 
Earth Cross Section for Meteoroids

For a projectile to hit a target it normally must impact within an area which is the cross-sectional area of the target. For a spherical body, this area is r2 where r is the radius of the sphere. However, in the case of a meteoroid or an asteroid impacting the Earth (or another planet), the appropriate cross- sectional radius is not the physical radius of the Earth, but it gravitational radius, which depends upon the impactor velocity.

Cross Section of Earth

This is because the Earth's gravity will attract an impactor that might be approaching on a near miss orbit. Imagine we have an impactor that in the absence of gravity has a space velocity v, and is on a trajectory with a distance Rg from the Earth's centre. Because of gravity the trajectory will curve toward the Earth and impact with a velocity V.

This impact will be tangential if Rg is the gravitational radius of the Earth (for the space velocity v (ie the body just impacts the planet). We can use the laws of conservation of momentum aned conservation of energy to determine Rg.

v Rg = V Rp (conservation of momentum)
v2/2 = V2/2 - G Me / Rp (conservation of energy)

where G is the universal gravitational constant. Solving these two equations simultaneously we find that:

Rg = Rp √[ 2 G Me / ( v2 Rp ) + 1 ]

The table below presents values of Rg (as a function of the space velocity), both in kilometres and as a fraction of the Earth's radius. Also shown are the fractional area, and the collision velocity.

Space
vel(km/s)
Collision
vel(km/s)
Effective
radius(km)
Fractional
radius
Fractional
area
2
4
5
6
8
10
15
20
25
30
35
40
45
50
11
12
12
13
14
15
19
23
27
32
37
42
46
51
36237
18942
15630
13494
10965
9571
7958
7309
6989
6809
6698
6625
6574
6538
5.68
2.97
2.45
2.12
1.72
1.5
1.25
1.15
1.1
1.07
1.05
1.04
1.03
1.02
32.26
8.81
6
4.47
2.95
2.25
1.56
1.31
1.20
1.14
1.1
1.08
1.06
1.05

Material Prepared by John Kennewell. © Copyright IPS - Radio and Space Services.



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