LOOKHEED P-38J November 24, 1992 In February 1937 the US Army Air Corps asked the American Aircraft industry to submit designs for an experimental pursuit having "the tactical mission of interception and attack of hostile aircraft at high altitude". Specifications called for a minimum true speed of 360 mph (579 km/h) at altitude and climb to 20,000 ft (6,096 m) within 6 minutes. In essence the Air Corps was asking for a major breakthrough in performance, since there were no engines of sufficient power to produce the expected results. Sixteen hundred (1,600) horsepower would be necessary and the only engine coming close to that kind of power was General Motors' small Allison Division V-1710-C8 which in February 1937 had yet to be tested at 1,000 hp. One of the solutions to this problem was to design and build a fighter using two Allisons. The result of the endeavor, was the creation of the LOOKHEED P-38 LIGHTNING. (The Great Book of World War II Airplanes, 1984, Bonanza Books) SPECIFICATIONS POWER PLANT o. Allison V-1710-111 (left side) and V-1710-113 (right side) o. 12-cylinder Vee-type liquid cooled, turbo-supercharged engines 1,425 hp each for take-off 1,425 hp at 26,500 ft (8,080 m) 1,600 hp in "war emergency" power at 28,700 ft (8,750 m) o. Curtiss electric three-bladed variable pitch constant Propeller diameter 11 ft 6 in (3,51 m) o. Internal fuel 410 US gal (341.4 Imp gal, 1,552 ltr) o. Auxiliary fuel tanks Two 75-300 US gal (62.5-250 Imp gal, 284-1,136 ltr) o. Oil tanks Two 13 US gal (10.8 Imp gal, 49 ltr) PERFORMANCE o. Maximum speed 414 mph (666 km/h) at 25,000 ft (7,620 m) o. Landing Speed 105 mph (169 km/h) o. Time to climb to 20,000 ft (6,100 m) 7 min o. Service Ceiling 44,000 ft (13,410 m) o. Range with 3,200 lb (1,452 kg) bombs 450 mls (720 km) o. Ferry range 2,600 mls (4,180 km) ARMAMENT o. One 20 mm M2 cannon with 150 rounds o. Four 0.50-in (12.7 mm) M2 machine guns with 500 rounds each o. Ten 5-in (127 mm) rockets o. Two 1,600 lb (726 kg) bombs WEIGHTS o. Empty 12,800 lb (5,810 kg) o. Gross 17,500 lb (7,940 kg) o. Max take-off 21,600 lb (9,800 kg) DIMENSIONS o. Span 52 ft (15.85 m) o. Length, level position 37 ft 10 in (11.53 m) o. Height, tip of propeller at top 9 ft 10 in (3.00 m) o. Undercarriage track 16 ft 6 in (5.03 m) o. Span of Tailplane 21 ft 9 in (6.63 m) o. Wing area 327.5 sq ft (30.4 m2) NOTE: The addition of AIRCRAFT AND ADVENTURE FACTORY (AAF) to the growing library of add-ons to MICROSOFT'S FLIGHT SIMULATOR, has greatly enhanced the abilities and capabilities to design and bring back to "LIFE" many a different planes. Even if certain limitations still exist with the software, I have tried to painstakingly recreate the P-38J to the best of AAF, MICROSOFTS' FS, and my abilities. I am very pleased with the final outcome, and hope to continue to improve my designing capabilities. The P-38 is the first of hopefully many more to come. Information I have received by word of mouth, stated that flying the P-38 was challenging, and somewhat more difficult to fly than other fighters of that era. Believe it, you will find that out to be true, as you attempt to fly the P-38J. Please remember to trim your elevators fairly quickly upon take off, if not the plane will make a very fast straight ascend. After trimming the elevators you will find the plane "fairly" easy to control. This design is copy protected. But it can be freely copied and distributed without modifications. If you have any comment, on how to further improve the P-38J please send me a note, either leaving me a note on LYNX BBS at (713) 746-3484, or dropping me a line at ÚÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄ¿ ³ Jim Goldman ³ ³ 574 E. Parktown ³ ³ Deer Park, Tx 77536 ³ ÀÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÄÙ ***HAVE A GOOD FLIGHT***