Lockheed Corporation

Lockheed T-33A Shooting Star

The Lockheed T‑33A Shooting Star is a jet trainer developed from the original P‑80 Shooting Star, the United States’ first operational jet fighter. In 1948 Lockheed modified the P‑80 airframe by adding a second seat for an instructor and lengthening the fuselage, creating a versatile two‑seat aircraft that entered service with the U.S. Air Force in 1949. Over 6,500 units were produced for more than 30 nations, making the T‑33 one of the most widely exported jet trainers of the Cold‑War era. Powered by a single Allison J33‑35‑35 turbo‑jet delivering 5,400 pounds of thrust, the aircraft achieved a maximum speed of 600 mph, a service ceiling of 46,000 ft, and a range of roughly 1,200 mi. Its straight‑wing design offered forgiving handling, while the tandem cockpit featured dual controls, basic avionics, and a hard‑point under each wing for weapons training. The T‑33A served not only as a trainer but also in reconnaissance, utility transport, and even light attack roles, shaping pilot proficiency worldwide. Its longevity, ease of maintenance, and role in transitioning pilots to more advanced supersonic jets cement its legacy as a cornerstone of post‑war military aviation.

Dimensions

Length
11.48 metre
Mass
5475 kilogram

Performance

Maximum Speed
521 knot
Service Ceiling
47500 foot
Range
1168 nautical mile

Production & History

Units Produced
5,871
First Flight
1948

Design & Classification

Country of Origin
Manufacturer
Lockheed Corporation
Developer
Lockheed Corporation
Nickname
Shooting Star
Military Designation
T-33A
Engine
J33-A-35
Wikidata ID
Q18175583