History
The success of the early Merlin-powered Mustangs led the Allies to appreciate their superior performance compared to the Allison-powered variants. However, concerns arose over the steady weight growth of the Mustang throughout its development into the P-51D/K models. These newer Mustangs found themselves outclimbed by Spitfires (by approximately 1,200 fpm) and outrolled by the Fw 190, which had nearly twice the roll rate. The RAF first approached North American in January 1943 regarding the possibility of a lightweight Mustang design, with the goal of reducing overall gross weight. This request eventually evolved into a joint program when the Army Air Forces formally initiated the contract and program management.
Three XP-51F prototypes, designated NA-105 by North American, were ordered on January 3, 1943, under MX-356 as the formal US Army project designation, before the first P-51D had even been produced. Consequently, the P-51E designation was skipped and never brought to fruition. In June 1943, the XP-51F contract was amended to include five aircraft (43-43332 through 43-43336) powered by the 1,380 hp V-1650-3. This was later changed to the 1,490 hp V-1650-7 while the aircraft were still under construction. The British also agreed to supply five 1,675 hp RM.14SM Merlin engines, which would power the final two aircraft of the amended order, designated XP-51G (NA-105A). The RAF requested one example of each model for its own testing.
Both the XP-51F and XP-51G completed their first flights in the summer of 1944. They were evaluated by the US Army Air Forces and the RAF, but neither type entered full-scale production. With experience gained from these aircraft, the USAAF decided to order two additional lightweight Mustang derivatives, bringing the total number of aircraft under the XP-51F/G contract to seven. The USAAF was particularly interested in evaluating a version powered by the new Allison V-1710-119 engine, which was designated XP-51J.
The XP-51J was essentially an XP-51F airframe mated to the V-1710-119 engine, which featured a two-stage supercharger and water injection. The engine was rated at 1,500 hp for takeoff and 1,720 hp with water injection at 20,700 feet. Installation of the new powerplant lengthened the fuselage by several inches and slightly increased the aircraft’s weight. Externally, the XP-51J could be distinguished by the absence of the carburetor air intake beneath the spinner. Instead, the carburetor air intake was relocated to the ventral radiator duct. The XP-51J retained the redesigned wings of the XP-51F, restricting internal armament to four 0.50-caliber machine guns. A dorsal fin extension was also fitted.
The first XP-51J (44-76027) was completed and made its maiden flight on April 23, 1945. However, the V-1710-119 engine was still immature and prohibited from operating at full power. It was flown again on December 19, 1945, before the aircraft was subsequently loaned to Allison Engine Plant at Indianapolis, Indiana, for additional engine testing and refinement on January 8, 1946. The second XP-51J (44-76028) was never flown and instead served as a source of spare parts to support continued testing of the first aircraft.
After many of the engine’s deficiencies had been corrected, the XP-51J resumed flight testing. It was first flown on January 29, 1946, and for the second time on January 31. However, with the war already at its end and the P-51H already entering full-scale production with the Packard-built Merlin V-1650-9, there was little justification for placing the XP-51J into production. Nevertheless, experience gained by Allison during the development of the V-1710-119 contributed to further refinements of the engine series, which ultimately powered all production Twin Mustangs from the P-/F-82E onward.