Bullet fired toward Earth from orbiting satellite

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Homework Statement



An Earth satellite is revolving in a circular orbit of radius 'a' with velocity 'v0'. A gun is in the satellite and is aimed directly towards the earth.A bullet is fired from the gun with muzzle velocity v0/2.Neglecting resistance offered by cosmic dust and recoil of gun,calculate maximum and minimum distance of bullet from the center of Earth during its subsequent motion.

Homework Equations





The Attempt at a Solution



Orbital speed of satellite is [itex]\sqrt{\frac{GM}{a}}[/itex]

Initial velocity of the bullet [itex]v_{i} = \sqrt{{v_o}^2+(\frac{v_0}{2})^2} = \frac{\sqrt{5}v_{0}}{2}[/itex]

Let P be the point at which bullet is fired and Q be point where distance is maximum/minimum.

Applying conservation of angular momentum at P and Q

[itex]mv_{i}a=mvr[/itex]

or , [itex]v = \frac{v_{i}a}{r} = \frac{\sqrt{5}}{2}\frac{av_0}{r}[/itex]

Applying conservation of mechanical energy at P and Q

[itex]\frac{1}{2}m{v_i}^2 - \frac{GMm}{a} = \frac{1}{2}m{v}^2 - \frac{GMm}{r}[/itex]

Solving the equations , I get [itex]3r^2-8ar+5a^2 = 0[/itex] which gives r =5/3a and a .

The answer i am getting is incorrect .

The correct answer given is 2a and 2a/3 .

I would be grateful if somebody could help me with the problem.
 
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Tanya Sharma said:

Homework Statement



An Earth satellite is revolving in a circular orbit of radius 'a' with velocity 'v0'. A gun is in the satellite and is aimed directly towards the earth.A bullet is fired from the gun with muzzle velocity v0/2.Neglecting resistance offered by cosmic dust and recoil of gun,calculate maximum and minimum distance of bullet from the center of Earth during its subsequent motion.

Homework Equations





The Attempt at a Solution



Orbital speed of satellite is [itex]\sqrt{\frac{GM}{a}}[/itex]

Initial velocity of the bullet [itex]v_{i} = \sqrt{{v_o}^2+(\frac{v_0}{2})^2} = \frac{\sqrt{5}v_{0}}{2}[/itex]

Let P be the point at which bullet is fired and Q be point where distance is maximum/minimum.

Applying conservation of angular momentum at P and Q

[itex]mv_{i}a=mvr[/itex]

or , [itex]v = \frac{v_{i}a}{r} = \frac{\sqrt{5}}{2}\frac{av_0}{r}[/itex]

Applying conservation of mechanical energy at P and Q

[itex]\frac{1}{2}m{v_i}^2 - \frac{GMm}{a} = \frac{1}{2}m{v}^2 - \frac{GMm}{r}[/itex]

Solving the equations , I get [itex]3r^2-8ar+ {\color{red}{5a^2}} = 0[/itex] which gives r =5/3a and a .
Check your algebra for that last term in your quadratic. Otherwise you've done fine up to that point.
 
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Hi gneill...

Sorry...I couldn't find any algebraic error .I redid the calculations . Maybe I am committing the same mistake again .

I keep on getting r=5a/3 and a .
 
Tanya Sharma said:
Hi gneill...

Sorry...I couldn't find any algebraic error .I redid the calculations . Maybe I am committing the same mistake again .

I keep on getting r=5a/3 and a .

Can't fix what we can't see...

Can you elaborate your derivation of the quadratic a bit?
 
[itex]\frac{1}{2}m{v_i}^2 - \frac{GMm}{a} = \frac{1}{2}m{v}^2 - \frac{GMm}{r}[/itex]

[itex]\frac{1}{2}m\frac{5}{4}\frac{GM}{a} - \frac{GMm}{a} = \frac{1}{2}m\frac{5}{4}\frac{a^2}{r^2}\frac{GM}{a} - \frac{GMm}{r}[/itex]

[itex]\frac{5}{8a}-\frac{1}{a} = \frac{5}{8}\frac{a}{r^2}-\frac{1}{r}[/itex]

[itex]\frac{-3}{8a} = \frac{1}{8r^2}(5a-8r)[/itex]

[itex]3r^2-8ar+5a^2 = 0[/itex] which gives [itex]r=5a/3 ,a[/itex]
 
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Tanya Sharma said:
[itex]\frac{1}{2}m{v_i}^2 - \frac{GMm}{a} = \frac{1}{2}m{v}^2 - \frac{GMm}{r}[/itex]

[itex]\frac{1}{2}m\frac{5}{4}\frac{GM}{a} - \frac{GMm}{a} = \frac{1}{2}m\frac{5}{4}\frac{a^2}{r^2}\frac{GM}{a} - \frac{GMm}{r}[/itex]
The LHS looks fine. But the velocity used on the RHS should be the velocity as obtained via the conservation of angular momentum:

##r \cdot v = a \cdot v_o## {angular momentum depends on the velocity component perpendicular to the radius vector}

##v = \frac{a}{r} v_o##

## v^2 = \left( \frac{a}{r} \right)^2 v_o^2## where: ##~~~v_o^2 = \frac{GM}{a}##
 
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Thanks gneill :smile:
 
Here's the source of your error:

Tanya Sharma said:
Applying conservation of angular momentum at P and Q

[itex]mv_{i}a=mvr[/itex]

The radial component of velocity does not contribute to angular momentum. This means that firing the gun doesn't change the bullet's orbital angular momentum.
 
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