- #1
marco12345a
- 13
- 0
When a rocket is launched, it starts not with velocity zero, but with the rotation velocity which the Earth gives it. Thus if a rocket is launched eastward, it requires a smaller boost (and if westward, a larger one) to achieve orbit. with a latitude of 31.1 degrees, cos(31degrees) 24902/24 = 393.11 ms/s
To escape velocity on Earth = (2G Mearth / r earth) = 11200ms-1
So the total velocity that needed for the rocket = 11200 - 393.11= 10806.99ms-1
I am trying to find the total energy that is needed for the rocket of 1000kg to escape velocity
i used the question
m = 1000 x 9.8 N
E= 1/2 m^2
= 5.84 X 10^10 J
my question is : as the further you are away from earth, there will be less gravity. So if i use that equation, would that be accurate assume there is no air friction and the mass of the rocket doesn't change due to the loss of fuel
To escape velocity on Earth = (2G Mearth / r earth) = 11200ms-1
So the total velocity that needed for the rocket = 11200 - 393.11= 10806.99ms-1
I am trying to find the total energy that is needed for the rocket of 1000kg to escape velocity
i used the question
m = 1000 x 9.8 N
E= 1/2 m^2
= 5.84 X 10^10 J
my question is : as the further you are away from earth, there will be less gravity. So if i use that equation, would that be accurate assume there is no air friction and the mass of the rocket doesn't change due to the loss of fuel