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F/A-18 Hornet
The F/A-18 "Hornet" is a single- and two-seat, twin
engine, multi-mission fighter/attack aircraft that can operate from either
aircraft carriers or land bases. The F/A-18 fills a variety of roles: air
superiority, fighter escort, suppression of enemy air defenses, reconnaissance,
forward air control, close and deep air support, and day and night strike
missions. The F/A-18 Hornet replaced the F-4 Phantom II fighter and A-7 Corsair
II light attack jet, and also replaced the A-6 Intruder as these aircraft were
retired during the 1990s.
The F/A-18 has a digital control-by-wire flight control system which provides
excellent handling qualities, and allows pilots to learn to fly the airplane
with relative ease. At the same time, this system provides exceptional
maneuverability and allows the pilot to concentrate on operating the weapons
system. A solid thrust-to-weight ratio and superior turn characteristics
combined with energy sustainability, enable the F/A-18 to hold its own against
any adversary. The power to maintain evasive action is what many pilots consider
the Hornet's finest trait. In addition, the F/A-18 was also the Navy's first
tactical jet aircraft to incorporate a digital, MUX bus architecture for the
entire system's avionics suite. The benefit of this design feature is that the
F/A-18 has been relatively easy to upgrade on a regular, affordable basis.
The F/A-18 has proven to be an ideal component of the carrier based tactical
aviation equation over its 15 years of operational experience. The only F/A-18
characteristic found to be marginally adequate by battle group commanders,
outside experts, and even the men who fly the Hornet, is its range when flown on
certain strike mission profiles. However, the inadequacy is managed well with
organic and joint tanking assets.
F/A-18A/B Hornet
While the general configuration of the YF-17 was retained, the F-18
became a completely new airplane. To meet the single-place fighter and attack
mission capability, full use was made of new technology in digital computers.
Coupled with cathode ray tubes for cockpit displays and appropriate controls
based on thorough pilot evaluations in simulators, a single airplane and
subsystems configuration for both missions was evolved
During development, two-place trainer versions were added, to be built in
limited numbers as TF/A-18s, intermingled with the basic F/As. Minimum changes
were made to incorporate the second cockpit, with the two-seat airplanes
retaining the ability to perform combat missions.
Making the first flight in November 1978, the F/A-18 and its two-place
derivative [subsequently redesignated the F/A-18B] underwent most of their
development testing at the Naval Air Test Center under the new single-site
testing concept. While much attention was focused on development problems, these
were largely typical of those in any new program, with their resolution being
part of the development process. For the most part, these occurred in the basic
aircraft hardware rather than in the digital electronic systems.
The original F/A-18A (single seat) and F/A-18B (dual seat) became operational
in 1983 replacing Navy and Marine Corps F-4s and A-7s. It quickly became the
battle group commander's mainstay because of its capability, versatility and
availability. Reliability and ease of maintenance were emphasized in its design,
and F/A-18s have consistently flown three times more hours without failure than
other Navy tactical aircraft, while requiring half the maintenance time.
The Hornet has been battle tested and has proved itself to be exactly what
its designers intended: a highly reliable and versatile strike fighter. The
F/A-18 played an important role in the 1986 strikes against Libya. Flying from
USS CORAL SEA (CV 43), F/A-18s launched high-speed anti-radiation missiles
(HARMs) against Libyan air defense radars and missile sites, effectively
silencing them during the attacks on Benghazi facilities.
F/A-18C/D Hornet
Following a successful run of more than 400 A and B models, the US Navy began
taking fleet deliveries of improved F/A-18C (single seat) and F/A-18D (dual
seat) models in September 1987. These Hornets carry the Advanced Medium Range
Air-to-Air Missile (AMRAAM) and the infrared imaging Maverick air-to-ground
missile. Two years later, the C/D models came with improved night attack
capabilities. The new components included a navigation forward looking infrared
(NAVFLIR) pod, a raster head-up display, night vision goggles, special cockpit
lighting compatible with the night vision devices, a digital color moving map
and an independent multipurpose color display.
F/A-18Cs have synthetic aperture ground mapping radar with a doppler beam
sharpening mode to generate ground maps. This ground mapping capability that
permits crews to locate and attack targets in adverse weather and poor
visibility or to precisely update the aircraft's location relative to targets
during the approach, a capability that improves bombing accuracy. New production
F/A-18Cs received the APG-73 radar upgrade radars starting in 1994, providing
more precise and clear radar displays.
The F/A-18C Nigh Attack Hornet has a pod-mounted Hughes AN/AAR-50 thermal
imaging navigation set, a Loral AN/AAS-38 Nite Hawk FLIR targeting pod, and GEC
Cat's Eyes pilot's night vision goggles. Some 48 F/A-18D two-seat Hornets are
configured as the F/A-18D (RC) reconnaissance version, with the M61A1 cannon
replaced by a pallet-mounted electro-optical suite comprising a blister-mounted
IR linescan and two roll-stabilized sensor units, with all of these units
recording onto video tape.
On the first day of Operation Desert Storm, two F/A-18s, each carrying four
2,000 lb. bombs, shot down two Iraqi MiGs and then proceeded to deliver their
bombs on target. Throughout the Gulf War, squadrons of U.S. Navy, Marine and
Canadian F/A-18s operated around the clock, setting records daily in
reliability, survivability and ton-miles of ordnance delivered.
The Navy announced 18 May 1998 that its East Coast F/A-18 squadrons will
relocate to Naval Air Station Oceana in Virginia Beach VA and Marine Corps Air
Station Beaufort in Beaufort, SC. The jets will move from Naval Air Station
Cecil Field in Jacksonville FL which was ordered closed by the 1995 Base
Realignment and Closure Commission. Nine operational squadrons and the Fleet
Replacement Squadron -- a total of 156 planes -- will move to Oceana. Two
squadrons totaling 24 planes will move to Beaufort. The first squadron will move
in the fall of 1998 and all 11 fleet squadrons and the Fleet Replacement
Squadron completed their moves by October 1999.
Throughout its service, annual upgrades to F/A-18 weapon systems, sensors,
etc. continued. The latest lot of the F/A-18C/D has grown to be far more capable
(night attack, precision strike, low observable technologies, etc.) than the
original F/A-18A/B; however, by 1991, it was becoming clear that avionics
cooling, electrical, and space constraints would begin to limit future growth.
Additionally, another operational deficiency was beginning to develop. As the
F/A-18C/D empty weight increased the aircraft were returning to the carrier with
less than optimal reserve fuel and/or unexpended weapons. The additional range
and "bring back" is not as essential to shore based operations. F/A-18A/B/C/D
aircraft will fly for years with the U.S. Marine Corps and eight international
customers: Australia, Canada, Finland, Kuwait, Malaysia, Spain, Switzerland and
Thailand. Although the F/A-18C/D's future growth is now limited, it will also
continue to fill a critical role in the U.S. Navy's carrier battle group for
many years to come and will be an excellent complement to the larger, longer
range, more capable F/A-18E/F Super Hornet.
F/A-18E/F "Super Hornet"
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 of the F/A-18 E/F Super Hornet:
- 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.
- 34 in. Fuselage Extension: The fuselage is slightly longer - the
result of a 34-inch extension.
- Two 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.
- 25% Larger Wing: A full 25 percent bigger than its predecessor,
Super Hornet has nearly half as many parts.
- 35% 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.
- 33% 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 (CVN 74).
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 Defence 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.
F/A-18G "Growler"
The EA-6B will begin retirement in the 2010 timeframe,
after a career that exceeded 40 years of deployments in support of USN, USMC,
and USAF strike forces. As of early 2000, Defense Department planning for
replacing the EA-6B Prowler include a scheme under which the Navy would buy an
F/A-18G "Growler" -- an F/A-18E/F modified for escort and close-in jamming. The
Air Force would provide standoff jamming with modified EB-52s or EB-1s, and
close-in jamming with unmanned air vehicles such as the Northrop Grumman Global
Hawk or General Atomics Predator.
Specifications |
Contractor |
Boeing [McDonnell Douglas Aerospace] and Northrop Grumman
(Airframe), General Electric (Engines), and Hughes (Radar)
|
|
F/A-18C/D Hornet |
F/A-18E/F Super Hornet |
Power Plant |
Two F404-GE-402 afterburning engines, each
in the 18,000 pound thrust class, which results in a combat
thrust-to-weight ratio greater than 1-to-1. Depending on the mission and
loading, combat radius is greater than 500 nautical miles.
| Twin F414-GE-400 engines, each in the
22,000 pound thrust class. On an interdiction mission, the E/F will fly up
to 40 % further than the C/D. |
Accommodations |
The F/A-18C and F/A-18E are single seat aircraft.
The D and F models are flown by two crew members.
The aft seat in the D and F may be configured with a stick and
throttle for the training environment (or without when crewed with a
Weapons System Officer). |
Performance |
F/A-18C maximum speed at level flight in altitudes of 36,089
ft. Mach 1.7 |
F/A-18E maximum speed at level flight in altitudes of 36,089
ft. Mach 1.6 |
Armament |
F/A-18C/D can carry up to 13,700 pounds of external ordnance.
Weapon stations include: two wingtip stations for Sidewinders; two
outboard wing stations for air-to-air or air-to-ground weapons; two
inboard wing stations for fuel tanks, air-to-air, or air-to-ground
weapons; two nacelle fuselage stations for AMRAAMs, Sparrows, or sensor
pods; and one centerline station for fuel or air-to-ground weapons.
M61
Vulcan 6-barrel rotary cannon with 520 rounds of 20mm ammunition is
internally mounted in the nose
AIM-9
Sidewinder AIM-7F
Sparrow AIM-120
AMRAAM AGM-65E
Maverick AGM-84
Harpoon AGM-88A
HARM MK82 10 CBU-87 10
CBU-89 GBU-12 GBU-24 JDAM B-57
or B-61 Nuclear bomb
|
F/A-18E/F can carry up to 17,750 pounds of external ordnance; two
additional wing store stations have been added.
|
Mission and Capabilities |
The F/A-18 Hornet can perform both air-to-air and air-to-ground
missions.
Cockpit displays and mission avionics are thoroughly integrated to
enhance crew situational awareness and mission capability in high threat,
adverse weather/night environments.
Cockpits are night vision goggle compatible.
Multi-Sensor Integration and advanced data link capabilities further
enhance situational awareness. |
The E/F model will be able to perform a strike tanker mission while
carrying a self-protection air-to-air missile loadout.
The E/F model will also have greater payload flexibility, increased
mission radius, survivability, payload bring back, and a substantial
avionics growth potential. |
Unit cost $FY98 [Total
Program] |
$39.5 million. |
$60 million |
Program Summary |
F/A-18A/B first entered operational service with the USN and USMC in
1982.
Since 1982, more than 1,458 F/A-18s have been procured for the USN and
USMC and for the armed services in Canada, Australia, Spain, Kuwait,
Switzerland, Finland, and Malaysia.
In 1987, the upgraded C/D model (with enhanced mission avionics) was
introduced and upgraded with a night/adverse weather mission capability,
On Board Oxygen Generating System, APG-73 Radar Upgrade, enhanced
performance F404-GE-402 engines, and upgraded mission computers. |
The first flight of the F/A-18E/F occurred in December 1995;
operational deliveries are scheduled for late 1999.
|
External Dimensions
|
F/A-18C/D |
F/A-18E/F |
Wing span |
11.43 m |
Wing span over missiles |
12.31 m |
Wing chord (at root) |
4.04 m |
Wing chord (at tip) |
1.68 m |
Wing aspect ratio |
3.52 |
Width, wings folded |
8.38 m |
Length overall |
17.07 m |
Height overall |
4.66 m |
Tailplane span |
6.58 m |
Distance between fin tips |
3.60 m |
Wheel track |
3.11 m |
Wheelbase |
5.42 m | |
Wing span over missiles |
13.62 meters |
Wing aspect ratio |
4.00 |
Width wings folded |
9.32 m |
Length overall |
18.31 m |
Height overall |
4.88 m | |
Areas
|
F/A-18C/D |
F/A-18E/F |
Wings, gross |
37.16 m2 |
Ailerons (total) |
2.27 m2 |
Leading-edge flaps (total) |
4.50 m2 |
Trailing-edge flaps (total) |
5.75 m2 |
Fins (total) |
9.68 m2 |
Rudders (total) |
1.45 m2 |
Tailerons (total) |
8.18
m2 | |
Wings, gross |
46.45 sq.
meters | |
Weights and Loadings |
F/A-18C/D |
F/A-18E/F |
Weight empty |
10,810 kg |
Maximum fuel weight: |
Internal (JP5) |
4,926 kg |
External: F/A-18
(JP5) |
3,053 kg |
CF-18 (JP4) |
4,245 kg |
Maximum external stores load |
7,031 kg |
Take off weight: |
Fighter
mission |
16,651 kg |
Attack mission |
Approx 23,541 kg |
Maximum |
Approx 25,401 kg |
Maximum wing loading (attack
mission) |
156,80
kg/kN | |
Weight, empty |
Design target |
13.387 kg |
Specification limit |
13.865 kg |
Maximum fuel weight: |
Internal |
6.531 kg |
External (JP5) |
4.436 kg |
Maximum external stores load
(JP5) |
8.051 kg |
T-O weight, attack mission |
29.937 kg |
Maximum wing loading |
620.0 kg/m2 |
Maximum power loading |
147.1 kg
/kN | |
Performance (At Maximum Takeoff Weight) |
F/A-18C/D |
F/A-18E/F |
Max level speed |
More than Mach
1.8 |
Max speed, intermediate power |
More than Mach
1.0 |
Approach speed |
134 knots |
Acceleration from 460 knots to 920 knots
at 10,670 m |
under 2 min |
Combat ceiling |
approx 15,240 m |
T-O run |
Less than 427 m |
Minimum wind over deck: |
Launching |
35 knots |
Recovery |
19 knots |
Combat radius, interdiction,
hi-lo-lo-hi |
290 nm |
Combat endurance, CAP 150 nm from
aircraft carrier |
1 h 45 min |
Ferry range, unrefueled |
More than 1,800
nm | |
Maximum level speed at
altitude |
more than Mach
1.8 |
Combat ceiling |
13,865 m |
Minimum wind over deck: |
- Launching
|
30 knots |
- Recovery
|
15 knots |
Combat radius specification:
Interdiction with four 1,000 lb bombs,
two Sidewinders, and two 1,818 liter (480 U.S. gallon: 400 Imp
gallon) external tanks, navigation FLIR and targeting FLIR:
Forward Looking Infra-Red hi-lo-lo-hi |
390 nm |
Fighter escort with two Sidewinders and
two AMRAAMs |
410 nm |
Combat endurance: maritime air
superiority, six AAMs, three 1,818 liter external tanks, 150 nm
from aircraft carrier. |
2h 15
min | |
Weapons Loads FA-18E
F/A-18
F/A-18E/F
Sources and Resources
- Hornet Hyperlink
USN PMA 265
- Hornet
Headlines NAVAIR newsletter
- F/A18-E/F
Super Hornet Main Navy Homepage
- Navy
Fact File: F/A-18 Hornet
- F/A - 18E/F PROGRAM
- Navy Acqusition Reform
- Naval
Technology -F/A-18E/F
- F/A-18
Hornet(C/D @ Boeing)
- F/A-18E/F
Super Hornet @ Boeing
- F/A-18
Hornet @ Northrop-Grumman
- F-18 @ GE
- F-18E @
GE
- HORNET! The F/A-18
Strike-Fighter [a pretty massive resource by Nicholas C. Zedlar]
- Boeing F-18 Hornet @
Fighter Tactics Academy
- Sea Serpent's
Online Strike Fighter Tactics manual
- F-18 Hornet (in French)
- Hornet Ball
- Hornet's Nest--Aviation Marine
Corps Style
- FA-18E/F vs.
A-6E comparison From: hornet265@aol.com (HORNET265)
- F/A-18E/F
DEVELOPMENT Congressional Record (Senate - October 23, 1991)
- F/A-18E/F
DEVELOPMENT Mr. D'AMATO - Congressional Record (Senate - May 05,
1992)
- F/A-18E/F
Mr. BOND -Congressional Record (Senate - June 30, 1992)
- SENATE
RESOLUTION 80--REGARDING TACTICAL FIGHTER AIRCRAFT PROGRAMS Mr. FEINGOLD
Congressional Record (Senate - April 30, 1997)
- THE
NAVY'S F/A-18E/F SUPER HORNET PROGRAM Mr. FEINGOLD Congressional
Record (Senate - March 23, 1998)
- 0204136N F/A-18
SQUADRONS FY98 R&D Budget Request
- F/A-18 E/F excerpts -
House National Security Committee Authorization Act for FY 1998
- F/A-18E/F
Update Chuck Spinney -- 01 Apr 1998
- F/A-18E/F --
Good to Go? Chuck Spinney -- 02 Apr 1998
- First
Super Hornet squadron ready to stand up Navy News Service 04/99
(Jan. 20, 1999)
- Super
Hornet enters operational evaluation NAVY WIRE SERVICE (NWS) - 7
June 1999 - The F/A-18E/F Super Hornet, entered operational evaluation
(OPEVAL) May 27. OPEVAL is scheduled to last six months and will be conducted
by an all-Navy independent test team.
- The
F/A-18E/F Super Hornet: A Test Pilot Dispels The Myths By CDR Rob
Niewoehner -- 14 April 1999 -- There has been a great deal of interest
recently in the press regarding the F/A-18E/F Super Hornet program, its
progress through the flight test phase, and the requirements for the airplane
in preparation for operational test.
- F/A-18
Super Hornet development testing complete The Weaponeer 10 June
1999 -- Following more than 270 test flights and more than 2,000 laboratory
test hours, the F/A-18 Advanced Weapons Laboratory (AWL) at the Naval Air
Warfare Center Weapons Division concluded several years' contribution to the
development of the F/A-18E/F Super Hornet.
- Super
Hornet Multi-Year Procurement Approved F/A-18 Public Affairs Office
October 28, 1999 -- President Clinton signed the fiscal 2000 Defense
Appropriations Bill. Included in the Bill is approval for a multi-year
procurement of 222 F/A-18E/F Super Hornets over the next five years.
- Final
LRIP 1 Super Hornet Delivered 6 Weeks Early F/A-18 Public Affairs
Office 10 Nov 1999 -- The last of the first 12 low-rate initial production
(LRIP) Super Hornets was delivered to the U.S. Navy on November 9, six weeks
ahead of schedule.
- "SUPER
HORNET" OPERATIONAL EVALUATION RESULTS ANNOUNCED February 15, 2000 - Chief
of Naval Operations, Adm. Jay Johnson, stated "The F/A-18E/F Super Hornet is
the cornerstone of the future of naval aviation. The superb performance
demonstrated throughout its comprehensive operational evaluation was just what
we expected."
- DoD
Special Briefing on "SUPER HORNET" Operation Evaluation Results February
15, 2000 -- The results were the best we could hope for. The airplane was
rated operationally effective and operationally suitable. This is the highest
grade the aircraft could receive. We believe we have a very mature aircraft
here; we believe we have an aircraft that's ready for the fleet.
- Workload
makes Hornet jets candidates for refurbishing, Stars and Stripes,
08 September 2000 -- The high operations tempo of recent years has pushed
hundreds of the Navy's F/A-18 Hornet attack jets toward the end of their
service life faster than anticipated and has sparked a 12-year, $878 million
program to keep the workhorse tactical aircraft flying.
http://www.fas.org/man/dod-101/sys/ac/f-18.htm
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