Dan-K... chwck your PM box. BTW- I have try to contact this museum where sole sample is preserved but email return as well wrong address [I copy\paste this]
Short history:
Curtiss designed a mixed-powered fighter as Model 99. It received the U.S. Navy type designation F15C-1. On 7 April 1944 Curtiss received a contract for the construction of three XF15C-1 prototypes. The assigned Bureau of Aeronautics serial numbers were 01213, 01214 and 01215. The new Curtiss fighter was fitted with a nose-mounted Pratt and Whitney R-2800 radial engine and an Allis-Chalmers J36 jet engine, which was in fact a licence built De Havilland H1-B Goblin from the U.K. The air intakes for the jet engine were placed in the wing roots. The exhaust of the jet engine was fitted under the fuselage. Further, the XF15C-1 was of modern all-metal construction, fitted with a teardrop shaped cockpit canopy and an undercarriage with a nose wheel.
The first XF-15C-1 made its maiden flight on 27 February 1945, still without the jet engine since this was still mounted in the bomb-bay of a converted TBF Avenger torpedo bomber for in-flight testing. Pilot on this occasion was Curtiss test pilot Lloyd Childs. On 3 May 1945, the first flight with both engines mounted could be made. Five days later, this machine crashed when on the landing approach the piston engine quitted because of fuel starvation. Curtiss test pilot Charles Cox was tragically killed in this crash.
The second XF15C-1 made its first flight on 9 July 1945, again flown by Lloyd Childs. All three prototypes were originally fitted with a fuselage mounted horizontal tail plane. To improve the flight characteristics, it was later reallocated to the top of the vertical stabilizer at the second and third machine. With the remaining two prototypes, operational evaluation tests were conducted until October 1946. Since the performances of the XF15C-1 were far below these of pure jet fighters, the program was terminated. Both prototypes were transferred to the Naval Air Test Centre at Patuxent River as general test aircraft, but eventually, they were hardly flown. No. 01214 was scrapped, but the last machine, no. 01215, still exists. It is now part of the collection of the Bradley Air Museum in Connecticut.
Technical details:
Power plant: one Pratt and Whitney R-2800-34W radial engine of 2100 hp and an Allis-Chalmers J36 jet engine of 1226 kg thrust
Sizes: wingspan 14.64 m
length 13.42 m
height 4.65 m
wing area 37.16 m2
Weights: empty weight 5737 kg
loaded weight 7543 kg (maximal 8481 kg)
Performances: max. speed 695 km/h at sea level ( 755km/h at 7715 m)
service ceiling 12,750 m
range 2228 km
Armament: four 20 mm cannons in the wings for the production version. The prototypes were unarmed
Accommodation: pilot
Bill- nice image

Is there any archive images?