Air Power Series>1:72 die-cast display model>F-105>HA2551
F-105F Thunderchief 63-8301, flown by Lt Col. Leo Thorsness, 355th TFW, 357th TFS, 17 April 1967
General Background
The F-105 earned the nickname Thud after the character Chief Thunderthud on the Howdy
Doody TV show. The main mission of the F-105G was the detection and destruction of North
Vietnamese SAMs that would then allow other aircraft to safely carry out their assignments. In
order for the F-105Gs to do this they were always “First In Last Out” and piloted by volunteers.
The F-105 was the only U.S. aircraft withdrawn from combat due to high losses. Having flown
20,000 sorties over Vietnam 382 of the 833 F-105s produced were lost.
The Aircraft
On April 19, 1967 Major Thorsness and Captain Johnson flew their F-105F Thunderchief 63-8301 along with their wingmen on a mission to destroy surface-to-air missile sites. They destroyed their first objective and attacking the second SAM the wingman was hit by ground fire and the crew bailed out. 63-8301 circled the parachutes to be able to give SAR their location. They spotted a MiG-17 and destroyed it. Low on fuel Thorsness began to leave but returned to take on four MiG-17s, destroying one while the other three fled.
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 (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 |