Mustang Mk.X | |
---|---|
Mustang Mk.X AM203 in the third configuration tested with a high-speed paint finish applied by Sanderson and Holmes, the coachbuilders in Derby, UK. | |
Role | Experimental aircraft |
Manufacturer | North American Aviation |
Built by | Rolls-Royce (modifications) |
First flight | 13 October 1942 |
Introduction | Experimental |
Primary users | Royal Air Force United States Army Air Forces |
Number built | 5 |
Developed from | North American P-51 Mustang |
The North American Mustang Mk.X, also known as the "Rolls-Royce Mustang") was an experimental variant of the North American Mustang I, (Model NA-73) an aircraft funded by the British Purchasing Commission and designed and developed by North American Aviation in 1940. It is distinct from the Merlin-powered P-51B/C that later followed. [1] The development proceeded incorporating a Rolls-Royce Merlin 65 medium-high altitude engine along with numerous modifications, in an experimental programme undertaken by Rolls-Royce in 1942.
The RAF had, following modifications by Lockheed at Speke to fit an oblique camera and other local British modifications, been actively using the Mustang I (Model NA-73) since early 1942 for Army Cooperation, tactical reconnaissance and as a fighter bomber and loved the aircraft's speed, range and performance.[ citation needed ]
In April 1942, the Royal Air Force's Air Fighting Development Unit (AFDU) tested the Allison V-1710-engined Mustang at higher altitudes and found it wanting above 18,000', but their commanding officer, Wing Commander Ian Campbell-Orde, was so impressed with its manoeuvrability and low-altitude speed that he invited Ronald Harker from Rolls-Royce's Flight Test establishment at Hucknall to fly it.[ citation needed ]
It was quickly evident that performance, although exceptional up to 15,000 ft (4,600 m), was inadequate at higher altitudes. This deficiency was due largely to the single-stage supercharged Allison engine, which lacked power at higher altitudes. Still, the Mustang's advanced aerodynamics showed to advantage, as the Mustang Mk.I was about 30 mph (48 km/h) faster than contemporary Curtiss P-40 fighters using the same Allison powerplant. The Mustang Mk.I was 30 mph (48 km/h) faster than the Spitfire Mk Vc at 5,000 ft (1,500 m) and 35 mph (56 km/h) faster at 15,000 ft (4,600 m), despite the latter having a more powerful engine than the Mustang's Allison. [2]
Above 15,000 ft (4,600 m) however, its performance fell off quite rapidly and at 20,000 ft (6,100 m) its maximum speed was 357 mph (575 km/h), which was slower than both the Spitfire Mk V and Messerschmitt Bf 109F. Its rate of climb also decreased significantly and it required eleven minutes to reach 20,000 ft (6,100 m) versus the Spitfire Mk V at seven. [3]
Nonetheless, Harker returned from his flight so enthusiastic, that he immediately phoned Ray Dorey, Head of Rolls-Royce's Experimental Division and asked how quickly a Merlin 61 from the Spitfire Mk IX could be fitted to the aircraft. Within 48 hours Dorey had consulted with Ernest Hives, head of Rolls-Royce and authorisation was given to proceed. [4]
Rolls-Royce's Chief Aerodynamic Engineer at Hucknall, W Challier, did aerodynamic calculations and estimated that the engine/airframe combination would result in a speed of 441 mph (710 km/h) at 25,600 ft (7,800 m).[ citation needed ]
Rolls-Royce began to affect the necessary conversion of four Mustangs designated Mustang Xs at Hucknall in June 1942. [5]
With a minimum of modification to the engine bay, the Merlin engine neatly fitted into the adapted engine formers. A smooth engine cowling with an additional "chin" radiator was tried out in various configurations as the two-stage Merlin required a greater cooling capacity than could be obtained with the standard Mustang radiator alone. The Merlin 65 series engine was used in all the prototypes as it was identical to the Merlin 66 powering the Spitfire Mk IX, allowing for a closer comparison. Due to the speed of the conversions, engines were often swapped from aircraft to aircraft as well as being replaced by newer units.[ citation needed ]
On 13 October 1942, AL975/G took to the air with Rolls-Royce's Chief Test Pilot Ronald Shepherd at the controls. A Merlin 65 [6] had been installed in the Mustang on a new engine mounting with the intercooler for the 2-speed, 2-stage Merlin mounted under the nose. All five development Mustang X aircraft had Merlin 65s, a medium/high altitude engine rather then the Merlin 61 high altitude engine. Visually, the Merlin Mustang differed from its Allison-engined predecessor by the removal of the latter's carburetor air intake above the nose. [7]
The high-altitude performance was a major advance over the Mustang I, with the Mustang X serial AM208 reaching 433 mph (697 km/h) at 22,000 ft (6,700 m) and AL975 tested at an absolute ceiling of 40,600 ft (12,400 m). Air Ministry official, Air Chief Marshal Sir Wilfrid Freeman (Chief Executive at the Ministry of Aircraft Production - MAP) lobbied vociferously for Merlin-powered Mustangs, insisting two of the five experimental Mustang Mk Xs be handed over to Carl Spaatz (commander of the USAAF in Europe) for trials and evaluation by the U.S. Eighth Air Force in Britain. In this, Lt Col. Hitchcock again played a key role. After sustained lobbying at the highest level, American production started in early 1943 of a North American-designed Mustang patterned after a P-51 Mustang prototype originally designated the XP-78 that utilised the Packard V-1650-3 Merlin engine replacing the Allison engine. [8]
The pairing of the P-51 airframe and Merlin engine was later designated P-51B for the model NA-102 (manufactured at Inglewood, California) or P-51C for the model NA-103 (manufactured at a new plant in Dallas, Texas from summer 1943). The RAF named both these models Mustang Mk.III. In performance tests, the P-51B achieved 441 mph (710 km/h) at 25,000 ft (7,600 m), and subsequent extended range with the use of drop tanks enabled the Merlin-powered Mustang version to be introduced as a bomber escort.[ citation needed ]
In June 1943, Rolls-Royce proposed to re-engine the Mustang with a Griffon 65, although the resultant "Flying Test Bed" (F.T.B.) would involve a dramatic redesign. Three surplus Mustang I airframes were allotted by the Ministry of Aircraft Production (MAP) and were dismantled in order to provide the major components for a mid-amidships installation of the more powerful Griffon engine, somewhat like the V-1710 Allison installation in the American Bell P-39 Airacobra and Bell P-63 Kingcobra. The project culminated in a mock-up, albeit with a Merlin 61 temporarily installed, serialed as AL960, that was examined by representatives from the Ministry in 1944, but was not given priority status. Further studies involving more powerful engines or turboprops were not given approval and the development contract was cancelled in 1945 and the mock-up was destroyed. [9]
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