|
As a broad rule of thumb, the fuel is about 90% the total mass of a space-bound rocket. The fuel tanks, engines, and the structures which hold it all together and control it are all in that remaining 10% of the total mass, and whatever is left is payload.
The Falcon 9 has a listed max payload of 13,150 kg or about 14.5 tons at surface gravity.
***
Another concidental rule of thumb is that the entry speed into the atmosphere in m/s is equal to the peak shock layer temperature in K. E.g. a spacecraft entering the atmosphere at 7.8 km/s would experience a peak shock layer temperature of 7,800 K. Air can become a plasma at temperatures in a range of 7,000 to 10,000 K - hotter than the "surface" of the sun. So a vehicle entering the atmosphere at ~7 to 10 km/s would ionize the atoms in the air, creating a plasma.
As for other emissions, the only I can think of would be to look at the meteor streak with a spectroscope and see if the spectral lines associated with Tungsten are there.
I'm sure the atmospheric entry and compression heating is producing a blackbody radiation signature which has a bandwidth of all wavelengths greater than 0. I.e. there is a non-0 chance of the thing emitting a photon of any conceivable energy, but the probability is like a bell curve with one short tail and one long tail. I suspect any light sensor pointed at an atmospheric entry will see it, because it will emit radio waves, microwaves, infra red, optical, ultra violet, hopefully not too much gamma.
|