The thrust to weight figures for the Meteor and 262 suprised me. I had always assumed they had similar power to weight, and that the superior aerodynamics of the 262 accounted for the speed difference.
The figures I was able to find, mostly from a couple of Jane's books, are:
Me262
Thrust
2x 1890lb at Sea Level at 560mph Fuel consumption 3680 lb/hr
2x 1605lb at sea level at 273mph fuel consumption 2920 lb/hr
Fuel Tankage 566 gallons
Range 650m
Speed 540mph at 20,000ft
Janes lists take off weight with 522 gallons of fuel, clean config 4 30mm guns and full ammunition as 15500lb
Meteor
Thrust
2x 2000lb static thrust at sea level fuel con 2360 lb/hr
2x 1550lb static thrust at sea level fuel con 1820 lb/hr cruising
Fuel tankage 330 gallons internal, 105 gallons fixed ventral tank
range 1340m
Speed various between 490 and 520mph. Also Bill Gunston gives the figure of 470mph at sea level
Weight. Janes lists 14000lb but doesn't say what configuration. The only reliable data I can find is 10684lb for an empty F8, which is presumably heavier than an F3
I don't know about the differences in thrust, wether 2000lb static is better or worse than 1890lb at 560mph. But I think in typical combat configuration, allowing for the much greater weight of fuel the 262 must carry, that the Meteor would be lighter than the 262, and should have a better thrust to weight ratio. I also presume the weight of the 30mm ammunition in the 262 would be greater than the 20mm in the Meteor, but I have no idea of the ammount the Meteor carried.
The 262 should still hold most of the advantages over the Meteor, but I don't think it's quite as bad as the figures suggest at first glance.
If anyone can provide definitive figures for any of this (SL speed of the 262 etc) then I would be gratefull).