Steve's Airshow World - Aircraft Factfile and Recognition Guide

Aircraft Factfile and Recognition Guide - F/A-18E/F Super Hornet

Background

The multi-mission F/A-18E/F "Super Hornet" strike fighter is an upgrade of the combat-proven night strike F/A-18C/D. The Super Hornet will provide the battle group commander with a platform that has range, endurance, and ordnance carriage capabilities comparable to the A-6 which have been retired. The F/A-18E/F aircraft are 4.2 feet longer than earlier Hornets, have a 25% larger wing area, and carry 33% more internal fuel which will effectively increase mission range by 41% and endurance by 50%. The Super Hornet also incorporates two additional weapon stations. This allows for increased payload flexibility by mixing and matching air-to-air and/or air-to-ground ordnance. The aircraft can also carry the complete complement of "smart" weapons, including the newest joint weapons such as JDAM and JSOW.

The Super Hornet can carry approximately 17,750 pounds (8,032 kg) of external load on eleven stations. It has an all-weather air-to-air radar and a control system for accurate delivery of conventional or guided weapons. There are two wing tip stations, four inboard wing stations for fuel tanks or air-to-ground weapons, two nacelle fuselage stations for Sparrows or sensor pods, and one centerline station for fuel or air-to-ground weapons. An internal 20 mm M61A1 Vulcan cannon is mounted in the nose.

Carrier recovery payload is increased to 9,000 pounds, and its engine thrust from 36,000 pounds to 44,000 pounds utilizing two General Electric F414 turbo-fan engines. Although the more recent F/A-18C/D aircraft have incorporated a modicum of low observables technology, the F/A-18E/F was designed from the outset to optimize this and other survivability enhancements.

The Hughes Advanced Targeting Forward-Looking Infra-Red (ATFLIR), the baseline infrared system for the F/A-18 E/F, will also be deployed on earlier model F/A-18s. The Hughes pod features both navigation and infrared targeting systems, incorporating third generation mid-wave infrared (MWIR) staring focal plane technology.

Although 41% interdiction mission range increase may be the most notable F/A-18E/F improvement, the ability to recover aboard with optimal reserve fuel and a load of precision strike weapons, is of equal importance to the battle group commander. The growth potential of the F/A-18E/F is more important to allow flexible employment strategies in future years. If an electronically scanned array antenna or another installation-sensitive sensor or weapon system becomes available, the F/A-18E/F has the space, power and cooling to accommodate it. Although the more recent F/A-18C/D aircraft have incorporated a modicum of low observables technology, the F/A-18E/F was designed from the outset to optimize this and other survivability enhancements. The all-F/A-18C/D/E/F air wing brings an increase in capability to the carrier battle group while ensuring the potential to take advantage of technological advances for years to come.

Features

90% Common F/A-18C/D Avionics: Avionics and software have a 90 percent commonality with current F/A-18C/Ds. However, the F/A-18E/F cockpit features a touch-sensitive, upfront control display; a larger, liquid crystal multipurpose color display; and a new engine fuel display.
Fuselage Extension: The fuselage is slightly longer - the result of a 34-inch extension.
Additional Multi-Mission Weapons Stations: Super Hornet has two additional weapons stations, bringing the total to 11. For aircraft carrier operations, about three times more payload can be brought back to the ship.
Larger Wing: A full 25 percent bigger than its predecessor, Super Hornet has nearly half as many parts.
Higher Thrust Engines: Increased engine power comes from the F414-GE-400, an advanced derivative of the Hornet's current F404 engine family. The F414 produces 35 percent more thrust and improves overall mission performance. Enlarged air inlets provide increased airflow to the engines.
Additional Internal Fuel: Structural changes to the airframe increase internal fuel capacity by 3,600 pounds, or about 33 percent. This extends the Hornet's mission radius by up to 40 percent.

Roll-out of the first Super Hornet occurred in September 1995, and it flew for the first time in November 1995, ahead of schedule and nearly 1,000 pounds under specified weight. In January 1997, the Super Hornet successfully conducted its initial sea trials on board the Navy's newest aircraft carrier, USS JOHN C. STENNIS (CVN74).

The Navy is planning to procure a minimum of 548 Super Hornets, and possibly as many as 1,000. These numbers could vary depending on the progress of the Joint Strike Fighter Program. As part of the Quadrennial Defense Review (QDR) production of the Super Hornet was cut from 1000 to 548 units. Production of the aircraft commenced in FY 1997, and it is expected to attain initial operational capability (IOC) in FY 2001. Twelve aircraft were funded in FY 1997; procurement numbers increase to 20 in FY 1998, 30 in FY 1999, and reach a final maximum rate of 48 per year in FY 2001.

On December 29, 2003 the U.S. Navy awarded Boeing a multiyear procurement contract valued at $8.6 billion for the production of an additional 210 F/A-18 Super Hornets. Under the terms of the multiyear contract, the Navy will purchase 42 aircraft in each of the fiscal years 2005 through 2009. The agreement provides the Navy with the flexibility to increase the quantity of aircraft on order by as many as six aircraft per year. Deliveries for aircraft purchased in the second multiyear will begin in fiscal year 2007.

Specifications: F/A-18E/F Hornet

Primary Function: Multi-role attack and fighter aircraft
Contractor: McDonnell Douglas
Unit Cost: $ 57 million
Propulsion: Two F414-GE-400 turbofan engines
Thrust: 22,000 pounds (9,977 kg) static thrust per engine
Length: 60.3 feet (18.5 meters)
Height: 16 feet (4.87 meters)
Maximum Take Off Gross Weight: 66,000 pounds (29,932 kg)
Wingspan: 44.9 feet (13.68 meters)
Range:
    Combat: 1,275 nautical miles (2,346 kilometers), clean plus two AIM-9s
    Ferry: 1,660 nautical miles (3,054 kilometers), two AIM-9s, three 480 gallon tanks retained
Ceiling: 50,000+ feet
Speed: Mach 1.8+
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-9X (projected), AIM 7 Sparrow,
AIM-120 AMRAAM, Harpoon, Harm, SLAM, SLAM-ER (projected),
Maverick missiles; Joint Stand-Off Weapon (JSOW); Joint Direct Attack Munition (JDAM);
Data Link Pod; Paveway Laser Guided Bomb; various general purpose bombs, mines and rockets.
Date Deployed: First flight in November 1995. Initial Operational Capability (IOC) in
September 2001 with VFA-115, NAS Lemoore, Calif.
First cruise for VFA-115 is onboard the USS Abraham Lincoln.

Sources: US Navy F/A-18 Hornet factfile, Federation of American Sciences