As a follow-on to the Mach 1 capable North American F-100 Super Sabre, the F-105 was also armed with missiles and a rotary cannon; however, its design was tailored to high-speed low-altitude penetration carrying a single nuclear weapon internally. First flown in 1955, the Thunderchief entered service in 1958. The single-engine F-105 could deliver a greater bomb load than some American heavy bombers of World War II such as the Boeing B-17 Flying Fortress and Consolidated B-24 Liberator. The F-105 was one of the primary attack aircraft of the Vietnam War; over 20,000 Thunderchief sorties were flown, with 382 aircraft lost including 62 operational (non-combat) losses (out of the 833 produced). Although less agile than smaller MiG fighters, USAF F-105s were credited with 27.5 kills.
During the war, the single-seat F-105D was the primary aircraft delivering heavy bomb loads against the various military targets. Meanwhile, the two-seat F-105F and F-105G Wild Weasel variants became the first dedicated SEAD platforms, fighting against the Soviet-built S-75 Dvina (NATO reporting name: SA-2 Guideline) surface-to-air missiles. Two Wild Weasel pilots were awarded the Medal of Honor for attacking North Vietnamese surface-to-air missile sites, with one shooting down two MiG-17s the same day. The dangerous missions often required them to be the “first in, last out”, suppressing enemy air defenses while strike aircraft accomplished their missions and then left the area.
When the Thunderchief entered service it was the largest single-seat, single-engine combat aircraft in history, weighing approximately 50,000 pounds (23,000 kg).[3] It could exceed the speed of sound at sea level and reach Mach 2 at high altitude. The F-105 could carry up to 14,000 lb (6,400 kg) of bombs and missiles. The Thunderchief was later replaced as a strike aircraft over North Vietnam by both the McDonnell Douglas F-4 Phantom II and the swing-wing General Dynamics F-111 Aardvark. However, the “Wild Weasel” variants of the F-105 remained in service until 1984 after being replaced by the specialized F-4G “Wild Weasel V”.
DIMENSIONS AND CAPACITY
CREW: 1 (Pilot) (Later versions became 2)
SIZE: LENGTH 64 ft 4 3⁄4 in (19.628 m),
WINGSPAN 34 ft 11 1⁄4 in (10.649 m),
HEIGHT 19 ft 8 in (5.99 m),
EMPTY WEIGHT 26,855 lb (12,181 kg)
MAX TAKE OFF WEIGHT: 52,838 lb (23,967 kg)
PERFORMANCE
SPEED: Mach 2.1 at 35,000 ft (10,668 m)
SERVICE CEILING: 48,500 ft (14,800 m)
RANGE: 676 nmi (778 mi, 1,252 km)
Armament:
Guns: 1 × 20 mm (0.787 in) M61A1 Vulcan 6-barreled Gatling cannon, 1,028 rounds
Hardpoints: 5 total: 4 × under-wing, 1 × centerline pylon stations plus an internal bomb bay with a capacity of up to 14,000 lb (6,400 kg) of ordnance,with provisions to carry combinations of:
Rockets:
LAU-32/LAU-59 rocket pods with 7 x FFARs each
Missiles:
AIM-9 Sidewinder air-to-air missiles
AGM-12 Bullpup air-to-surface missiles
AGM-45 Shrike anti-radiation missiles
Bombs:
M117 and Mark 80 series of general-purpose bombs
Cluster munitions of various types, including CBU-24