I think the ship would probably be finished in space, to make sure the hull is air-tight and calibrate it for space.
I like TGT's explanation that what we saw in the trailer was an all-up systems test before being broken down into component sections, boosted into orbit, assembled, and completed.
I like TGT's explanation that what we saw in the trailer was an all-up systems test before being broken down into component sections, boosted into orbit, assembled, and completed.
Also consider the fact that firing an engine like that on the Earth's surface would lay waste to a vast area of land, to say nothing about the radiation a sustained fusion reaction would put out.Correct me if I'm wrong
- Assuming an impule engine can accelerate the Enterprise to c/2, whre c is the speed of light.
- Assuming the Enterprise has 600,000 metric tonnes, which is 6.0 x 10^11 g, the energy required to get it into a 36,000 Km orbit is:
delta Eg = Eg (orbit) - Eg (ground), where Eg = Gravitational Potential Energy
Given:
Radius of Earth = 6,378 km ~= 6.4 x 10^6 m
Orbit = 3.6 x 10^7 m
= mgh (orbit ) - mgh (ground) = mg(hg - ho)
= 6x10^11g * 9.81 m/s/s * ( 3.6 x 10^7 m - 6.4 x 10^6 m)
Eg= 1.74 x 10^20 J
Withoug going into relativity, and using simple kinematics (v =c/2, rlativistic effects can be ignored), to get the Enterprise from rest velocity to c/2 we need the following energy:
Ek = 0.5*m*v^2 = 0.5*m*(c/2)^2 = 0.125*m*c^2 = 6.75 x 10^27
Ek = 6.75 x 10^27 J
Now, as you can see the energy required to get to half the speed of light is 10 million times grater than to get into standard geosyncronous orbit. Think about that.