F/A-18 C / D Hornet
Primary Function: Multi-role attack and fighter aircraft
Contractor: Prime: McDonnell Douglas; Major Subcontractor: Northrop
Unit Cost: $29 million
Propulsion: Two F404-GE-402 enhanced performance turbofan engines
Thrust: 17,700 pounds static thrust per engine
Length: 56 feet (16.8 meters)
Height: 15 feet 4 inches (4.6 meters)
Maximum Take Off Gross Weight: 51,900 pounds (23,537 kg)
Wingspan: 40 feet 5 inches (13.5 meters)
Range Combat: 1,089 nautical miles (1252.4 miles/2,003 km), clean plus
two AIM-9s
Ferry: 1,546 nautical miles (1777.9 miles/2,844 km), two AIM-9s plus three 330
gallon tanks
Ceiling: 50,000+ feet
Speed: Mach 1.7+
Crew:
A, C and E models: One
B, D and F models: Two
Armament: One M61A1/A2 Vulcan 20mm cannon;
External payload:
AIM 9 Sidewinder,
AIM 7 Sparrow,
AIM-120 AMRAAM,
Harpoon,
Harm, SLAM, SLAM-ER,
Maverick missiles;
Joint Stand-Off Weapon (JSOW); Joint Direct Attack Munitions (JDAM); various
general purpose bombs, mines and rockets.
Date Deployed:
First flight - November 1978
Operational - October 1983 (A/B models); September 1987 (C/D models);