F-105 "Thunderchief" - Lackland AFB - San Antonio, Texas
Posted by: BruceS
N 29° 22.993 W 098° 38.054
14R E 535493 N 3250499
Fighter-bomber aircraft on display near the west gate at Lackland Air Force Base.
Waymark Code: WM3C15
Location: Texas, United States
Date Posted: 03/12/2008
Views: 10
F-105
"Thunderchief"
Design work began on the F-105 in 1951. It was to be a single seat
supersonic fighter-bomber capable of carrying a heavy load of conventional and
nuclear bombs at high speeds over a long range. The first of two YF-105A
prototypes powered by a Pratt and Whitney J57 engine, exceeded mach 1 during its
initial flight of 22 October 1955. The production version, F-105B fighter
bomber was powered by the Pratt and Whitney J75-P-3 engine, developing 25,000
lbs of thrust with afterburner. The first "B" model flew on 26 May 1956.
The F-105B was the heaviest single-seater to enter service with the USAF,
grossing over 40,000 lbs and capable of carrying 8,000 lbs of bombs internally
and 4,000 lbs externally. The F-105D was first issued to tactical air
force units in 1961. Initially serving in the United States and eventually
in Germany. In 1965, F-105Ds went into action in Vietnam in the tactical
ground attack role. The F-105D is known as the "Thud" and was used
extensively in Southeast Asia as a fighter bomber. Production of the
latter ended in 1964 after several hundred had been built. This aircraft
was flown by LT COL James Risner, Commander, 67th Tactical Fighter Squadron,
18th Tactical Fighter Wing, while on TDY to Danang AB, Republic of Vietnam,
January through September 1965. Colonel Riser was shot down and captured
by the North Vietnamese 16 September 1965. Eight years later, he was
released along with other POWs as a result of the 28 January 1973 agreement.
Manufacturer: Republic |
Quantity Produced: 833 |
Wing Span: 34 ft 11 in |
Speed: 1,254 mph |
Length: 67 ft |
Power Plant: Pratt & Whitney J75-P-19W Engine |
Height: 19 ft 8 in |
|
Max T-O Weight: 40,000 lb |
|
Information from sign in front of aircraft.