- Description:
- The two-place
T-33 "Shooting Star" was designed for training pilots
already qualified to fly propeller-driven aircraft.
It was
developed from the single-seat
F-80 fighter by lengthening the fuselage about three
feet to accommodate a second cockpit.
Originally designated the TF-80C, the T-33 made its
first flight in 1948. Production continued until 1959
with 5,691 T-33s built in the United States. The
US Navy also
acquired the type and had it modified for blue-water
operation as the TV-2 "Sea
Star".
The T-33
became the most widely used jet trainer in the world,
and was soon dubbed the "T-Bird". In addition to its use
as a trainer, the T-33 has been used for such tasks as
drone director and target towing, and in some countries
even as a combat aircraft. The RT-33A, a
reconnaissance version made primarily for use by foreign
countries, had a camera installed in the nose and
additional equipment in the rear cockpit.
Manufactured under license
in both Japan (T-33 "Wakataka" or "Young Hawk")
and Canada (CT-133 "Silver
Star") total production of
all types exceeded 6,500 aircraft, making the
T-33 one of the world's best-known aircraft. It
has served with the air forces of more than 30 different
nations over several decades.
The Shooting Star continued to be used by United
States Air National Guard units until 1994.
Versions of the T-33 are still in service with
the armed forces of Bolivia, South Korea, Mexico,
Paraguay, and Thailand.
About 50 are in the hands
of private operators, mostly in the United States.
- Specifications:
|
"The T-Bird"
T-33A Two-Seat Jet Trainer |
|
Crew |
2
for flight instruction; or 1 for flight currency
training |
|
Armament |
Normally none; or two .50 caliber guns for training |
|
Dimensions |
Length: 37ft 1in |
|
Height: 11ft 8in |
|
Wingspan: 38ft 10in |
|
Wing
Area: 234.8 sq ft |
|
Weights |
Empty: 8,897lb |
|
Gross: 16,800lb |
|
Maximum: 18,100lb |
|
Engine: 1,650lb |
|
Engine |
One
Allison J33-A-24 Turbojet Engine; Double entry
centrifugal compressor, none straight flow
combustion chambers, and a single stage turbine. |
|
Fuel
Capacity |
677.5 US gallons |
|
Performance |
Engine Thrust: 5,400lbs |
|
Range: 1,025 miles |
|
Cruise Speed: 455mph (395kts) |
|
Max
Speed: 600mph (505kts) or 0.8 MACH |
|
Max
Climb:
4,870 ft/min |
|
Ceiling:
48,000ft |
|
Structure Limit: +7.3G and -3G |
|
Spins are Prohibited
Inverted Flying is prohibited |
Click here for Cockpit Photos in the
T-33 Photo Gallery
|