F-100D Super Sabre Triple Zilch, 20th TFW, 1957 (1:72)

The "D" variant was the ultimate version of the F-100 with 1,274 aircraft being produced. The production of the F-100 ended in August 1959. The F-100D arrived in Southeast Asia in 1962 with its primary mission being close air support and ground attack within South Vietnam. This role was eventually taken over by the A-7 Corsair II. The aircraft became affectionately known as ��_The Hun��_, short for ��_one HUNdred��_. The last F-100 left Vietnam in July 1971 but not before 242 of these aircraft was lost. The ��_Hun��_ was eventually replaced by the F-4 Phantom II and the F-105 Thunderchief.

HISTORY SPECIFIC TO THIS AIRPLANE WILL BE POSTED HERE SOON.

Specifications for the F-100D

Primary function
Fighter-Bomber

Engine
1 X Pratt & Whitney J57-P-21/21A turbojet, 10,200 lb.st. dry and 16,000 lb.st. with afterburning.

Dimensions
Wingspan 38 ft 9 in
Length - 50 ft 0 in
Height - 16 ft 2 3/4 in
Wing area - 400 sq. ft.

Performance
Maximum speed - 770 mph at sea level (clean), 864 mph (Mach 1.3) at 36,000 ft (clean).
Initial climb rate - 19,000 ft/min. An altitude of 35,000 ft could be attained in 2.3 minutes.
Service ceiling - 36,100 ft, combat ceiling 47,700 ft, absolute ceiling 50,000 ft.
Normal range - 534 mi, maximum range 1,995 mi.
Fuel capacity ��_ 1,739 US gallons internally, total of 2,139 gallons if maximum external fuel is carried.

Weights
Empty - 21,000 lbs
Gross - 28,847 lbs
Maximum T/O - 34,832 lbs

Armament
4 X 20-mm Pontiac M-39 cannon
6 X under-wing pylons for up to 7,040 lbs of bombs, fuel tanks, or rockets.
1 X MK-28 or Mk-43/57/61 nuclear weapon could be carried.
In later versions, 4 X AIM-9B/E/J Sidewinder air-to-air infrared homing missiles could be carried.