Northrop YF-17 Cobra

🇺🇸 UNITED STATES
RETIRED
Lightweight day-fighter prototype — direct ancestor of the F/A-18 Hornet family
🚀
MAX SPEED
Mach 1.95
2,092 km/h
⛰️
CEILING
15.2 km
50,002 ft
🗺️
RANGE
1,480 km
919 mi
📅
FIRST FLIGHT
1974
✈️
Speed Ranking
#153 fastest of 262 aircraft in this database

✈️ Full Specifications

DesignationYF-17 Cobra
ManufacturerNorthrop
Country🇺🇸 United States
First Flight1974
Retired1980
Crew1
Length17.1 m (56.1 ft)
Wingspan10.6 m (34.8 ft)
Height4.6 m (15.1 ft)
Empty Weight7,800 kg (17,199 lb)
Max Takeoff Weight11,340 kg (25,005 lb)
Max Speed (Mach)1.95
Max Speed2,092 km/h (1,300 mph)
Service Ceiling15,240 m (50,002 ft)
Range1,480 km (919 mi)
Engine2 × General Electric YJ101-GE-100
Thrust (each)Dry 32.5 kN · AB 67 kN
Production2

🌐 Operators

✈️ United States Air Force✈️ NASA

🔁 Variants

  • YF-17 — Lightweight Fighter prototype
  • Seed for the F/A-18 Hornet program (1976+)

⚔️ Armament

Designed for 1× M61A1 Vulcan 20mm + AIM-9 Sidewinder loadout Prototypes never carried live weapons

Overview

The Northrop YF-17 Cobra was developed in the early 1970s as Northrop’s entry in the U.S. Air Force’s Lightweight Fighter (LWF) competition. The YF-17 lost the contest to General Dynamics’ YF-16 in January 1975, but in losing it found a new life: the U.S. Navy adopted a developed version of the design as the F/A-18 Hornet, eventually becoming one of the most prolific naval fighters of the late 20th century and the basis for today’s Super Hornet and EA-18G Growler.

Design & Development

The YF-17 grew out of Northrop’s P-530 Cobra studies of the late 1960s — an attempt to apply the lessons of the F-5 Tiger II into a higher-performance day fighter. Northrop chose a twin-engine layout (two General Electric YJ101 turbojets) for redundancy at the cost of complexity. The design featured leading-edge root extensions (LERX) blended into the wing, twin canted vertical stabilisers, and a relatively conventional fuselage.

Two prototypes were built and flew in 1974. While both the YF-16 and YF-17 met the LWF performance requirements, the YF-16 was faster, lighter, and (controversially) used a derivative of the same F100 engine as the F-15 Eagle — a powerful logistics argument. The YF-17 was selected by the Navy in May 1975 for further development into a carrier-capable strike fighter, becoming the F/A-18.

Operational History

The first YF-17 (72-1569) flew on June 9, 1974, with Northrop test pilot Hank Chouteau at the controls. The aircraft demonstrated supersonic performance on its second flight and exceeded Mach 1 in a climb during the LWF flyoff. Both prototypes accumulated over 280 test flights before the LWF down-select to the F-16 in January 1975.

The two YF-17 airframes were transferred to NASA’s Dryden Flight Research Center, where they served as testbeds into the early 1980s. Both are now in museums — one at the Western Museum of Flight in Torrance, California, the other at NASA Dryden / Edwards AFB.

Legacy

The YF-17 lost its battle but won its war. As the F/A-18 Hornet, the design entered service in 1983, was the foundation of the F/A-18E/F Super Hornet (which entered service in 2001), and gave rise to the EA-18G Growler electronic attack aircraft. As of 2026, more than 1,500 Hornet-family aircraft have been built across the Hornet and Super Hornet families — vastly more than the F-16-line production numbers would suggest from the LWF source-selection decision.

References

  • USAF Lightweight Fighter program documentation, 1974–1975
  • Northrop YF-17 Cobra program history, Northrop archives
  • “Hornet: McDonnell Douglas F/A-18” by Robert F. Dorr
✈️
Sean

Aviation enthusiast and curator of the Supersonic Aircraft Encyclopedia. Sean has been passionate about different kinds of flight since he was little and maintains detailed specs and history for every aircraft featured on this site.

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