Careful what you say.Type 407 and Type 421 Wellington Mk V
Three were built, designed for pressurised, high-altitude operations using turbocharged Hercules VIII engines.
Type 432 Wellington Mk VI
One high-altitude prototype only.
Type 449 Wellington Mk VIG
Two production aircraft only.
Comments....? It seems you made some variants up
127 in total. Not many, as the Stirling/Halifax/Lancaster heavies were coming online in numbers, but it's certainly a hell of a lot more more than six. I don't make things up.VICKERS WELLINGTON (High-altitude bomber variants) - The Vickers Wellington 1C airframe provided basis for adaptation as a high-altitude bomber, conforming to Specification B.23/39. Requirement was for a three-man crew, ability to bomb from 35,000 ft (10,668 m) or above, and to have an endurance of more than nine hours. Pressurisation was to begin at 15,000 ft (4,572 m), the altitude specified for cruise to and from the target.
Vickers Wellington V: Two prototypes (R3298, R3299) by conversion of Mk 1C airframes, ordered in May 1939, as Vickers Type 407 with high-altitude Bristol Hercules VIII engines. Rear turret retained but pressure cell extended into nose, replacing forward turret, and accommodated rear gunner during high-altitude portion of flight. First prototype flown September 1940 with 1,400 hp Hercules Ills (as Type 421); second prototype had 1,650 hp Hercules VIIIs and smaller 'blister' dome for pilot's head in place of longer canopy on first prototype. Production batch of 30 Mk Vs ordered to Specification 17/40, in compliance with Operational Requirement OR. 94, to have Hercules VIII (Type 426) or Hercules 38 (Type 448) engines. One only (W5796) completed as Mk V; 20 as Mk VI (see below) and nine cancelled.
Vickers Wellington VI: Similar to Mk V, with 1,280 hp Rolls-Royce Merlin 60 engines.
First of production-batch Mk Vs (W5795, Vickers Type 431), completed as prototype Mk VI and flown in late 1941, followed by 19 more from Mk V contract and 44 from new production contract (for 100; others cancelled) placed in 1941. Standard FN20A turret retained, but gunner in pressure cell at all times, using periscopic sight in underside of fuselage. Basic type (28 aircraft) as Vickers Wellington VIA (Vickers Type 442), but final 35 were Vickers Wellington VIG (Type 449) without rear turret, and with Oboe blind-bombing aid. Two Vickers Wellington VIG used operationally by No 109(SD) Sqn, and others to train crews in use of Oboe. Max speed, 300 mph (483 kmlh). Service ceiling, 38,500 ft (11,735 m). Range, 2,275 mis (3,661 km) with 15,000-lb (6,804-kg) bombs. Empty weight, 20,280 Ib (9,200 kg). Gross weight, 30,450 Ib (13,812 kg). Span, 86 ft 2 in (26.26 m). Length, 61 ft 9 in (18.82 m). Wing area, 840 sqft (78.04 m2).
Regarding
...see above.Again, I have to wonder which parallel universe`s Wellington are you talking about... 6804 kg, where that figure from, is it including inflation rates of the past 70 years or what?
You're quite right, I meant the Armstrong Whitworth Whitley - but as forAvro Whitley didn`t exist, you are thinking of the Armstrong Whitworth Whitley. I believe only a handful were around of them and were seen as obsolate types at the beginning of the war - other than its considerable bombload, it had little to offer (and in this respect it as soon outdone by Heinkel 111s : the H-4 was capable of lifting 2800 kg, the H-5 3600 kg)
I believe only a handful were around of them and were seen as obsolate types at the beginning of the war
THAT Whitley? Notice the emboldened section. 1,500 both ordered AND produced AFTER the start of the war does argue against "a handful" and "were seen as obsolete"...ARMSTRONG WHITWORTH AW.38 WHITLEY - The Armstrong Whitworth Whitley was designed under the direc-tion of J Lloyd to the requirements of Specification B.3/34 for a five-seat 'heavy bomber' replacement for the Heyford and Hendon, to carry a 2,500-lb (1,135-kg) bomb load over 1,250 mis (2,010 km) at 225 mph (362 km/h) at 15,000 ft (4,575 m). First of two prototypes (K4586) with 795 hp Tiger IX engines flown at Whitley, Coventry, aerodrome on March 17, 1936. Second prototype (K.4587) with Tiger XIs flown February 11, 1937.
Armstrong Whitworth Whitley I: First contract for 80 Armstrong Whitworth Whitley Mk Is placed 'off the drawing board' in June 1935. First example flown December 23, 1936; deliveries to No 10 Sqn, RAF, on March 9, later to Nos 51 and 78 Sqns. Tiger IX engines; armament of single 0.303-in (7.7-mm) Lewis gun each in front (AW. or Nash and Thompson) and rear (AW.) manual turrets. Production termi-nated at 34th aircraft.
Armstrong Whitworth Whitley II: Final 46 aircraft on initial contract completed with 920 hp Tiger VIIIs with two-speed superchargers, to Specification B.21/35. Deliveries mid-1938, to Nos 7, 51, 58 and 97 Sqns. One Armstrong Whitworth Whitley II (K7243) test-bed for AS Deerhound 21-cyl air-cooled radial engine, flown Jan 1939-March 1940.
Armstrong Whitworth Whitley III: Second production batch of 80, to Specification B.20/36, similar to Armstrong Whitworth Whitley Mk II but with powered Nash and Thompson single-gun nose turret and retractable ventral 'dustbin' turret with two O.303-in (7.7-mm) Brownings. Bomb-bay and racks modified for larger bombs. Deliveries second half of 1938 to replace Mk Is and Us and also to Nos 77, 97, 102 and 166 Sqns. Early marks of Armstrong Whitworth Whitley from Nos 51 and 58 Sqns flew first RAF Nickel (leaflet) raid over Germany on night of September 3/4, 1939.
Armstrong Whitworth Whitley IV: Final 40 aircraft on second production contract (additional to 80 Mk Ills) fitted with Merlin in-line engines and extra fuel tanks. Prototype (converted Mk I K7208) first flown at Hucknall on February 11, 1938; first production Armstrong Whitworth Whitley IV flown on April 5, 1939 with Merlin IVs; final seven aircraft had 1,070 hp Merlin Xs and designated Armstrong Whitworth Whitley IVA.
Armstrong Whitworth Whitley V: Contracts placed in 1938 for 312, in 1939 for 150 and in 1940 for 1,150 Armstrong Whitworth Whitleys, of which 1,466 completed as Armstrong Whitworth Whitley Mk V and 146 as Armstrong Whitworth Whitley Mk VII (see below). As Mk IV with Nash and Thompson powered tail turret mounting four 0.303-in (7.7-mm) Browning guns; 15-in (38.1-cm) rear fuselage extension to improve rear gunner's field of fire; modified fin shape; wing leading-edge rubber de-icers and fuel capacity increased to 837 Imp gal (3,805 1). First production Mk V flown August 8, 1939, and initial deliveries to No 77 Sqn in September. Many Armstrong Whitworth Whitley Vs (and some earlier marks) used as glider tugs, with towing gear in place of rear turret or fitted beneath rear fuselage, and as para-troop transports; also used to drop agents into occupied territory. Fifteen Armstrong Whitworth Whitley Mk Vs transferred (with civil registrations) to BOAC for Gibraltar-Malta supply flights, 1942/43.
Armstrong Whitworth Whitley VII: Total of 146 Armstrong Whitworth Whitley Mk VII built on final production contract, plus some Mk V conversions, to serve with Coastal Command squadrons on maritime reconnaissance duties, carrying ASV Mk II radar (with four dorsal radar masts plus lat-eral and underwing aerials), sixth crew member and extra fuel in bomb bay and fuselage to a total of 1,100 Imp gal (5,000 1) for a range of 2,300 mis (3,700 km). Initial CC squadrons were Nos 502 (GR) and 612 (GR), using standard Armstrong Whitworth Whitley Vs from 1940 and 1941 respectively, with Armstrong Whitworth Whitley VIIs introduced 1942.
The Luftwaffe didn't have any strategic bombing doctrine. That isn't false. The RAF did, but unfortunately had aircraft for it that while suitable for the carrying-out of that doctrine were as of 1939-41 just about marginal for it at that time but had bigger and better in design and testing while those fought on. Of course the Luftwaffe possessed more and more suitable medium bombers - I DO believe I said that - and they DID use them to wage two strategic bombing campaigns.Again, the whole arguement originated that you`ve claimed the RAF had a strategic doctrine and bomber force suitable for it at/before the start of the war, and the LW didn`t. I pointed out the notion is simply false.
The LW actually possessed more and more suitable, long ranged medium bombers than the RAF`s BC at the start of the war. This kind of emphasis on long range bombers capable of waging strategic bombing, and considerable pre-war development for noctural bombing devices surely wasn`t only incidental.
But "pre-war development of noctural bombing devices" does NOT argue that anyone in the RLM or LW was specifically planning STRATEGIC bombing pre-war - it argues that the LW fully intended to carry out round-the-clock tactical/operational level bombing with their tactical bombers as opposed to being stupid enough as to develop a parallel but separate day/night capability like the RAF had. It's exactly what I said above in my example of the B-17 - the ability to fly to Hawaii, Alaska and Panama brought Germany within easy reach from England...but it doesn't indicate the US was planning to bomb Germany from England in 1934, does it? By YOUR logic it would.
The mechanical failure rates in 1944 are NOT opinion, they are recorded fact. Have you checked them out?This opion of yours is in direct contrast with British intterogations of captured He 177 crew in early 1944, who express great confidence in the big Heinkel`s reliability.
(all British tech. specs. and material taken from here - http://www.jaapteeuwen.com/ww2aircraft/index.htm)