- #1

- 37

- 0

**1. Say that an electron is heading towards the Earth from the sun with an initial known velocity v. And we know that at Earth's surface the magnetic field is given by B1. This B varies as (R1/R2)^2 where R1 is the radius of the earth. How can I find the location in space, R3/R1, where R3 is the distance where the electron's cyclotron radius equals the distance from earth?**

**2. w = qB/m**

R = v/w ( - cos (wt) in x direction + sin (wt) in y direction )

R = v/w ( - cos (wt) in x direction + sin (wt) in y direction )

**3. So I started by assuming that**

- since B varies with (R1/R2)^2 then

B = B1 (R1/R2)^2

I'm not sure if this is a right assumption...

But anyhow,

since we know B now then

w = [ q B1

- since B varies with (R1/R2)^2 then

B = B1 (R1/R2)^2

I'm not sure if this is a right assumption...

But anyhow,

since we know B now then

w = [ q B1

**(R1/R2)^2 ] / m**then I took this w and plugged it into

**R = v/w ( - cos (wt) in x direction + sin (wt) in y direction ) giving me**

R = (v R2^3 m)/(qB1R1^3) ( -cos ((

Now I don't know what to do because of the t in the cos and sin function...

R = (v R2^3 m)/(qB1R1^3) ( -cos ((

**[ q B1**t) + sin (**(R1/R2)^2 ] / m)****(**t) )**[ q B1****(R1/R2)^2 ] / m)**Now I don't know what to do because of the t in the cos and sin function...

I thought of squaring both sides to get cos^2+sin^1 = 1 but I don't think that would work out...