Don't know where to begin?
---Ignore the question and write down whatever formula that might be useful, even odd ones.
---Look at what you know, then at your equations
---Form any links
---Look back at the question and what it is asking.
Ok the question is to do with gravity, so perhaps Newton's Law of Gravitation might be useful;
F = GmAmB / r2
Then perhaps his Second law of motion;
F=ma
Well we know the masses and radii so this looks good. First take the link that;
mAa = GmAmE
So that for some object A in a gravitational field arround B it will experience a force accelerating it downwards. This is g hence;
gE = GmE / r2
For Earth we can just plug the data in for its mass, and a radius at a given point, let's say the Earths surface. Thus we know g on Earth.
For Uranus, we are told it's 18 times more massive, and its radius is 3.7 times bigger. Thus we can rewrite our formula for gravitational accelaration on Uranus as;
gU = 18GmE / (3.7*rE)2
Simple really (you can expand the denominator and remove the numerical co-efficent as a fraction of 18 and that is your ratio of Earths gravitational accelaration to Uranus's. ;)
+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
The next bit is somewhat more tricky unless you've done A level or A level equivilent calculus;
Ok raising a massive in a mass in a gravitational field means doing work against the gravitational pull of the planet. Hence we can write the expression;
w = Integ{ F } ds
Where the work done (w) is the infintesimal sum of all the little movements 'up' in the gravitational field. Now say we want to raise this object an infinite distance in the gravitational field, well that's going to be tricky. But that is our end limit of intergration. Assuming we are going to raise the mass from the planets surface (in this case Uranus which is 3.7 times greater than Earths radius) that makes our other limit. Hence our equation looks like;
w = IntegInfinity3.7rE{ F } ds
F = GmAmE / r2
and our direction of motion for the ds is actually in the radial direction from Uranus's centre (I won't go into conservative forces here), we will denote this 'dr'. Hence;
w = (1800/1369)*IntegInfinity3.7rE{ GmAmE / r2 } dr
NOTE: the ratio in bold is that ratio I was talking about ealier. I have removed it from the intergration brackets because it doesn't change with the intergration varible r. You can probally appreciate that I could have also taken out G, and the product of the masses at this stage as well should I have wanted to.
Anyhow you'll note that this intergrates to;
w = [ -(1800/1369)*GmAmE / r ]Infinity3.7rE
NOTE: 1 / r is the same as r-1.
Now you can just evaluate the numerical amount of work it takes to raise the object to infinity.
Question: What is work a quantity of? and how is this linked to this escape speed we want to find? Well work is a form of energy, hence you'll appricate that;
Work Done = Kinetic Energy
Kinetic energy is 1/2 mAv2 where v is its velocity. Hence you might be able to appricate that;
w = 1/2 mv2
sqrt{ (2w / mA) } = v
This v is your escape velocity, because if an object had this velocity, then it has enough energy to escape the pull of gravity that the planet would provide. Preaty neato huh?
In practice this is only a lower limit due to air resistance etc. and the rotation of the planet would also create an accelrating frame of referance for the object at the equator, but those are trival in most circumstances.
Hope that helps!
Haths