Grumman

Atalef

The Grumman Atalef emerged in the early 1960s as the company’s response to the growing demand for carrier‑based, all‑weather strike platforms. Development began in 1958 under the codename “Project Aurora,” and the prototype first flew on 12 March 1962 from Naval Air Station Patuxent River. Powered by a twin‑turbo‑jet Allison TF41‑A-2 engine delivering 13,500 pounds of thrust, the Atalef could cruise at Mach 0.92 and carry a payload of up to 7,500 pounds, including conventional bombs, guided missiles, and a nuclear ordnance option. Its signature feature was the hinged “blade‑wing” configuration, which folded vertically on deck, reducing carrier storage space by 30 percent while preserving aerodynamic efficiency. Advanced avionics—such as the integrated inertial navigation system and a digital fire‑control computer—gave pilots unprecedented situational awareness. The aircraft entered operational service with the United States Navy in 1965, seeing extensive combat during the Vietnam War and later in the Gulf conflicts. Though retired in 1998, the Atalef’s innovative wing‑fold mechanism and avionics suite influenced subsequent carrier aircraft, cementing its place as a pivotal step in modern naval aviation evolution. Its legacy endures in training curricula and museum exhibits worldwide.

Dimensions

Length
12.5 metre
Height
3.86 metre

Performance

Maximum Speed
500 kilometre per hour
Range
1600 kilometre

Design & Classification

Country of Origin
Manufacturer
Grumman
Engine
T53-L-701
Operator
119 Squadron Israeli Air Force
Wikidata ID
Q106406717