Now look at the Meteor III which was hopping around Europe from January (?) 1945.
Powered by 2 × de Havilland (Halford H-1) Goblin DGn.1 turbojets, rated at 2,300 lb st (10,23 kN) dry each. Other differences are a rearward-sliding and jettisonable canopy, and fuel capacity of 325 Imp gal (390.3 US gal; 1477,5 liters). The middle 180 were G.41D aircraft with Rolls-Royce (Power Jets W.2B/37) Derwent RD.1 turbojets, rated at 2,000 lb st (8,90 kN) dry each and supplied with internal fuel that could be supplemented by 105 Imp gal (126.1 US gal; 477,3 liters) in an optional but non-jettisonable ventral tank. The last 15 were G.41E aircraft with Derwent RD.1 turbojets in longer nacelles. In other respects, the G.41D version of the Meteor F.Mk III was dimensionally identical to the Meteor F.Mk I but differed in details such as its empty weight of 8,810 lb (3.996 kg), max take-off weight of 13,300 lb (6.033 kg), max level speed of 495 mph (797 km/h) at 30,000 ft (9.145 m) declining to 458 mph (737 km/h) at sea level, cruising speed of 350 mph (563 km/h) at optimum altitude, range of 1,340 miles (2156 km), maximum rate of climb at sea level of 3,980 ft (1.213 m) per minute, and service ceiling of 44,000 ft (13.410 m).
Number built: 210
(From Frans Bonnes excellent website)
495 mph at alt is not bad at all, the range is okay, sl speed is just fine, climb is so so.
The 262 has 540 mph at 20K, ceiling 40K,climbs 3,937 ft per min at sl, and to some 19,685 ft in 6 min 48 sec.
Climb to 19,685 ft in 6 min 48 sec weights 9742 lb typical,
14080 lb max, thrust from 2 × Junkers Jumo 109-004B-1/2/3 turbojets, rated at 1984 lb st (8.83 kN) dry each. Range was 652 miles.
So, why not the Meteor? It's not quite as fast, - well maybe at 30K
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But seriously the only threat possible for the 262 apart from the 163 of course
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