North American
F-100
Super Sabre
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Photo: Robert Deering 10/18/2012
National Museum of the USAF
Wright-Patterson AFB (FFO)

Dayton, Ohio

The North American F-100 Super Sabre is an American supersonic jet fighter aircraft that served with the United States Air Force (USAF) from 1954 to 1971 and with the Air National Guard (ANG) until 1979. The first of the Century Series of USAF jet fighters, it was the first USAF fighter capable of supersonic speed in level flight. The F-100 was designed by North American Aviation as a higher performance follow-on to the F-86 Sabre air superiority fighter.

Adapted as a fighter-bomber, the F-100 was supplanted by the Mach two-class F-105 Thunderchief for strike missions over North Vietnam. The F-100 flew extensively over South Vietnam as the air force's primary close air support jet until being replaced by the more efficient subsonic LTV A-7 Corsair II. The F-100 also served in other NATO air forces and with other U.S. allies. In its later life, it was often referred to as the Hun, a shortened version of "one hundred".


F-100F
Photo: Robert Deering 10/18/2012

National Museum of the USAF
Wright-Patterson AFB (FFO)

Dayton, Ohio

F-100D
Photo:Robert Deering 9/3/2013

Highland Lakes Squadron CAF Museum
Burnet Municipal Airport (BMQ)

Burnet, Texas

Variants

YF-100A - Prototype, model NA-180 two built, s/n 52-5754 and 5755.

YQF-100 - Nine test unmanned drone versions

F-100A- Single-seat day fighter; 203 built, model NA-192.

RF-100A ("Slick Chick") - Six F-100A aircraft modified for photo reconnaissance in 1954. Unarmed, with camera installations in lower fuselage bay. Used for overflights of Soviet Bloc countries in Europe and the Far-East. Retired from USAF service in 1958, the surviving four aircraft were transferred to the Republic of China Air Force and retired in 1960.

F-100B - See North American F-107

F-100BI - Proposed interceptor version of F-100B, did not advance beyond mock-up.

F-100C - Seventy Model NA-214 and 381 Model NA-217. Additional fuel tanks in the wings, fighter-bomber capability, probe-and-drogue refueling capability, uprated J57-P-21 engine on late production aircraft. First flight: March 1954; 476 built.

TF-100C - One F-100C converted into a two-seat training aircraft.

F-100D - Single-seat fighter-bomber, more advanced avionics, larger wing and tail fin, landing flaps. First flight: 24 January 1956; 1,274 built.

F-100F - Two-seat training version, armament decreased from four to two cannon. First flight: 7 March 1957; 339 built.

DF-100F - This designation was given to one F-100F that was used as drone director.

NF-100F - Three F-100Fs used for test purposes, the prefix "N" indicates that modifications prevented return to regular operational service.

TF-100F - Specific Danish designation given to 14 F-100Fs exported to Denmark in 1974 in order to distinguish these from the 10 F-100Fs delivered 1959–1961.

QF-100 - Another 209 D and F models were ordered and converted to unmanned radio-controlled Full Scale Aerial Target drones and drone directors for testing and destruction by modern air-to-air missiles used by current U.S. Air Force fighter jets.

 

F-100J - Unbuilt all-weather export version for Japan

 

F-100K - Unbuilt design study for a two-seat F-100F powered by a J57-P-55 engine

 

F-100L - Unbuilt design study for a single-seat F-100D powered by a J57-P-55 engine

 

F-100N - Unbuilt version with simplified avionics for NATO customers

 

F-100S - Proposed French-built F-100F with Rolls-Royce Spey turbofan engine

SPECIFICATIONS: (F-100D) PERFORMANCE:
Span:  38 ft 9 in (11.81 m)
Length: 
50 ft (15 m)
Height:  16 ft 2.75 in (4.9467 m)
Empty Weight:  
21,000 lb (9,525 kg)
Gross Weight: 
28,847 lb (13,085 kg)
Crew:
1
Maximum speed: 924 mph (1,487 km/h, 803 kn)
Cruising speed:
Range:
1,995 mi (3,211 km, 1,734 nmi)
Service ceiling:
50,000 ft (15,000 m)
Engines: 1 × Pratt & Whitney J57-P-21/21A afterburning turbojet engine, 10,200 lbf (45 kN) thrust dry, 16,000 lbf (71 kN) with afterburner
Armament: Four M-39 20mm cannons with 175 rounds and a maximum of 5,000 lbs. of external stores
   
SOURCE: Wikipedia  
   
1959 DOD Aircraft
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