Air Power Series>1:72 die-cast display model>F-105>HA2507
F-105D Thunderchief 62-4301, 466th TFS Hill AFB, Utah "My Karma"
General Background
The Republic F-105 Thunderchief first entered service in 1958. It had been designed for high-speed low-level penetration to deliver a nuclear bomb but was converted to deliver conventional payloads. It was the heaviest U.S. single-engined fighter ever made and could carry a greater bomb load than the B-17, B-24 or B-29. Best known for its action in Vietnam the F-105 flew over 20,000 combat missions with the loss of 382 aircraft out of the 833 produced.
The Aircraft
USAF S/N 62-4301 is an F-105D-31-RE, one of 610 F-105Ds built by Republic Aviation in Farmingdale, New York. It was delivered to the USAF on April 25, 1963 and assigned to the 8th Tactical Fighter Wing (PACAF), Itazuke AB, Japan. In May, 1964 it was assigned to the 41st Air Division (PACAF), at Yokota AB, Japan, where it was stationed until January, 1968 when it was sent to the 18th Tactical Fighter Wing (PACAF), Osan AB, Korea. While with the 18th TFW it made two brief combat tours with the 355th TFW at Takhli AB, Thailand, and achieved an unofficial ground kill of an IL-28 bomber during one of the tours. From April to August, 1972 it was here at McClellan for maintenance. From here it went to the 507th Tactical Fighter Group (AFRES), Tinker AFB, Oklahoma, and finally in July, 1980 to the 466th Tactical Fighter Squadron (AFRES), Hill AFB, Utah. It was flown to the museum on January 16, 1984.
Specifications :
| Nick Names: | Ultra Hog, Super Hog, Iron Butterfly, Lead Sled, Thud |
| Role: | Fighter/Bomber |
| User Countries: | U.S.A |
| Crew: | (1) pilot |
| Performance | |
| Engine: | (1) Pratt & Whitney J75-P-19W turbojet, rated at 17,200 lb.s.t. dry and 26,500 lb.s.t. with afterburner |
| Maximum Speed: | 1,420 mph at 38,000 ft |
| 1,372 mph at 36,000 ft | |
| 1,122 mph at 50,000 ft | |
| 836 mph at sea level | |
| Stall speed: | 208 mph |
| Initial Climb Rate: | 34,500 fpm (clean) |
| Service Ceiling: | 32,100 ft |
| Combat Ceiling: | 48,500 ft |
| Maximum Ceiling: | 50,000 ft |
| Combat Range: | 778 miles |
| Maximum Range with full external fuel: | 2,208 miles |
| Weight | |
| Emptyt: | 27,500 lbs |
| Combat: | 35,637 lbs |
| Gross: | 48,400 lbs |
| Maximum Take/Off: | 352,546 lbs |
| Fuel | |
| Normal Internal Fuel Load: | 1,160 US gallons |
| Internal Weapons Bay: | 390 US gallon auxiliary tank |
| Optional 450 or 650 US gallon external tanks on the fuselage centerline | |
| Plus a 450 US gallon tank on each of the inboard under-wing pylons | |
| Dimensions | |
| Wing Span: | 34 ft 11 in. |
| Length: | 64 ft 3 in. |
| Height: | 19 ft 8 in. |
| Wing Area: | 385 sq. ft. |
| Armament: | (1) 20-mm M61A1 rotary cannon with 1028 rounds (fire rate 6,000 rpm) |
| Up to 8,000 lbs of ordnance could be carried in the internal weapons bay | |
| An additional 6,000 lbs of ordnance could be carried on (4) under-wing pylons and (1) rack under the fuselage center-line | |
| Up to (4) AIM-9 Sidewinder missiles for self-defense | Up to (4) AGM-12 Bullpup (not very effective in Vietnam) | (1) Mk 28 or Mk 43 nuclear weapon |
| Up to (2) 3,000 lb bombs | |
| Up to (5) 1,000 lb bombs | |
| Up to (16) 750 lb bombs | |
| Mk 77 napalm, ECM pods, 2.75 in. rockets |