- #1
dopey9
- 32
- 0
Identical spacecraft s A and B each of mass m are orbiting the Earth in different orbits...they both have the same perigee and at t=0 spacecraft A hits spacecraft B from behind
before impact speed of A was V[a]
and B was V and both a distance R from the centre of the earth
After the collision the two spacecraft stick together as a single lump of wreckage
im trying to find an expression for the angular momentum of the wreckage in terms of m, R, V[a], V...i was wondering if anyone knows what formulas i require to work out the expression...if anyone could please possibly show me how to solve this becuase I am finding it mind boggling thankz
before impact speed of A was V[a]
and B was V and both a distance R from the centre of the earth
After the collision the two spacecraft stick together as a single lump of wreckage
im trying to find an expression for the angular momentum of the wreckage in terms of m, R, V[a], V...i was wondering if anyone knows what formulas i require to work out the expression...if anyone could please possibly show me how to solve this becuase I am finding it mind boggling thankz