| The
AH-1W Super Cobra is the US Marine's attack helicopter. It is
supplied by Bell Helicopter Textron and entered service in 1985. As
well as the US Marine Corps, the Super Cobra is operational with the
Turkish Land Forces and the armed forces of Taiwan. The AH-1W was
deployed, with astonishing success, in support of Operation Iraqi Freedom in March 2003.
In 1966, the DOD
contracted with Bell Helicopter, Inc. for 1,100 AH-1G
aircraft, which logged more than 1 million flight hours in Vietnam.
Subsequently, the USMC desired a twin engine AH-1G; thus, the SEA
COBRA (AH-1J) was developed. The United States Marine Corps then identified a need for more armaments; thus, the AH-1T upgrade
was initiated. This aircraft had an extended tailboom and fuselage
and an upgraded transmission and engines.
The AH-1 is fully
capable of performing its attack mission in all weather conditions.
Additional missions include direct air support, antitank, armed
escort, and air to air combat. The TOW missile targeting system uses
a telescopic sight unit (traverse 110º, elevation 60º/+30º), a
laser augmented tracking capability, thermal sights and a FLIR to
allow for acquisition, launch, and tracking of all types of TOW
missiles in all weather conditions. The Cobra also uses a digital
ballistic computer, a HUD, Doppler nav, and a low speed air data
sensor on the starboard side for firing, and has in-flight
boresighting. External stores are mounted on underwing external
stores points. Each wing has two hardpoints for a total of four
stations. A representative mix when targeting armor formations would
be eight TOW missiles, two 2.75-in rocket pods, and 750x 20-mm
rounds. The gun must be centered before firing underwing stores.
Armored cockpit can withstand small arms fire, and composite blades
and tailboom are able withstand damage from 23-mm cannon hits.small
arms fire, and composite blades and tailboom able to withstand
damage from 23-mm cannon hits.
The Marines depend
on attack helicopters to provide close-in fire support coordination
in serial and ground escort operations. Such support is required
during amphibious ship-to-shore movements and subsequent shore
operations within the objective area. AH-1 is designed for the
following tasks:
* Armed escort for
helicopters carrying personnel and cargo
* Landing zone fire
suppression support
* Visual armed
reconnaissance
* Target marking and
direction for high-performance attack aircraft
* Convoy escort and
fire suppression for ground units
* Operations from
air capable ships
* Point target
attack of threatening armor
* Self-defense and
protection of helicopters carrying personnel and cargo from
threatening air-to-air weapon-equipped helicopters
By the early 1980s,
USMC aircraft inventory was declining due to attrition; a fully
navalized helicopter was sought. In 1983, the USMC contracted with
Bell for 44 AH-1Ws. The AH-1W Super Cobra is a day/night marginal
weather Marine Corps attack helicopter. The AH-1W is
a two-place, tandem-seat, twin-engine helicopter capable of land- or
sea-based operations. The AH-1W provides fire support and fire
support coordination to the landing force during amphibious assaults
and subsequent operations ashore. The AH-1W distinguished itself
with its more powerful T700-GE-401 fully marinized engines and
advanced electronic weapons capability. The AH-1W can fire TOW,
Hellfire, and Sidewinder missiles and can be outfitted with Zuni
rocket launchers.
The AH-1W is
operated in eight composite HMLA squadrons composed of 18 AH-1 and 9
UH-1 aircraft. The AH-1W is outfitted with a Night
Targeting System/Forward Looking Infrared Radar that provides laser
rangefinding/designating and camera capabilities.
The AH-1W is
operated in eight composite HMLA squadrons composed of 18 AH-1 and 9
UH-1 aircraft. The Marine Corps deployed 4 of 6 active force
squadrons (48 AH-1Ws) to Southwest Asia during Operation Desert
Shield/Desert Storm. These helicopters destroyed 97 tanks, 104
armored personnel carriers and vehicles, 16 bunkers and 2
antiaircraft artillery sites without the loss of any aircraft. The
deployment required no additional augmentation to squadron support
personnel and only one Bell Helicopter technical representative.
AH-1G Cobra
Bell Helicopter won
the competition for an interim fast armed escort helicopter in March
1966, against the Sikorsky S-61 and the Kaman HH-2C Tomahawk.
The original AH-1G
prototype (Bell N209J) had fully retractable skids.
The AH-1G Cobra [or
"Snake"]
was first deployed to Vietnam in September 1967. The Cobra's primary
mission was to give fire support to troop carrying Hueys. Its
trial-by-fire introduction to service as the AH-1G in Vietnam
immediately provided ground commanders with air superiority without
the wait of calling in the Air Force. The narrow 38 inch wide
airframe presented a much more difficult target than it's
derivative, the 100 inch wide UH-1 "Huey". During the
Vietnam War, the AH-1G Cobra was used extensively in a variety of
missions ranging from armed escort and reconnaissance to fire
suppression and aerial rocket artillery. The Cobra was often used effectively when paired with an
unarmed OH-6A Cayuse "Loach" or OH-58A Kiowa light
observation helicopter or a UH-1H "Nighthawk".
During the early
1970s, the Army conducted a series of tests in Ansbach, Germany. The
tests were to determine the suitability of air cavalry elements and
the AH-1G Cobra, in particular, to operate in an antitank role in
the European environment. These tests demonstrated that antiarmor
helicopter teams, properly employed and trained, could achieve high
ratios of armored vehicles destroyed for every missile-firing
helicopter lost. Armed scout and attack helicopters--especially when
operating in nap-of-the-earth and nighttime environments--clearly
were shown to have the required survivability and to be viable and
essential elements of conventional mid- to high-intensity warfare.
Thus the way was paved for the development of the modern attack and
scout helicopters and the doctrinal principles that would take Army
aviation into the next century.
The AH-1G Cobra was armed with 2.75 inch (70mm) Folding Fin Aerial Rockets (FFARs)
in M158 seven-tube or M200 19-tube rocket launchers, used so
effectively at An Loc in 1972. The Cobra had a chin-turret on the
M28/M28A1 armament subsystem. The chin-turret mounted the M134
7.62mm minigun and the M129 40mm grenade launcher. The AH-1G could
also be armed with the M134 minigun in fixed side-mounting M18/M18A1
gun pod, and the port (left) side mounting M195 20mm automatic gun
on the M35 armament subsystem. The AH-1G could also mount the XM118
smoke grenade dispenser.
Some early model
AH-1G/AH-1Q Cobras mounted either two M134 miniguns or two M129
grenade launchers in a M28A1 chin-turret (TAT-141). Because of
problems with the ammunition feed systems, the twin-gun
configuration was discontinued. The Cobra was first employed to
Vietnam with the 1st Cavalry Division (Airmobile) in August 1967.
The Cobra's primary mission was to give fire support to troop
carrying Hueys. The AH-1G/AH-1Q Cobras were powered by a single
Lycoming T53-L-13 1400 shp turbine engine, and had a speed of 196
mph (170 knots), almost twice the speed of the UH-1 Huey. Both the
AH-1G and AH-1Q Cobra used the M73 reflex sight. The Cobra performed
it's job so well it was possible for the first time for Slicks and
gun ships to operated as true air calvary.
The AH-1G was
equipped with the CONFICS (Cobra Night Fire Control System) and the
SMASH (Southeast Asia Multi-Sensor Armament Subsystem for Huey
Cobra) systems to provide the Cobra with the capability of
detecting, identifying, and targeting ground targets during day or
night operations.
AH-1J
Sea Cobra
The Marines also operated armed Hueys in
Vietnam, and ordered their own version of the Cobra in May 1968. The
USMC desired a twin engine AH-1G; thus, the SEA COBRA (AH-1J) was
developed. Featuring the Pratt and Whitney Twinpac T400 engine (two
900-hp turboshaft engines coupled together) giving an overall
increase in installed power, the AH-1J Sea Cobra included a new nose
turret gun, the three barrel XM-197 20mm and other improvements.
While development and production of the first 49 ordered were under
way, the Marines obtained 38 AH-1Gs from the Army.
After initial training of Marines by the
Army, Marine Huey Cobras first became operational in April 1969 with
VMO-2 in Vietnam. In December 1969, the AH-1Gs were transferred to
HML-367. After flight tests beginning that same month and subsequent
trials, the first AH-1Js joined them in February 1971, entering
combat the following month. AH-1Js, including those of HMA-369,
participated in Southeast Asia operations until final withdrawal and
continued as the Marine's attack helicopter afterwards, a total of
67 being delivered. The Marine AH-1Gs became the reserve helicopter
attack squadron's aircraft.
AH-1Q Cobra
True to the arguments of those who feared
for the AH-56 Cheyenne program, the funds for that program were
almost immediately cut following the 1966 decision to buy the AH-1G,
and the AH-56 Cheyenne eventually died. Ten prototypes were
completed before the program was terminated August 9, 1972 due to
delayed development, rising costs, and the appearance of two
competitive company-funded initiatives by Sikorsky and Bell. The
helicopter's mission would eventually be assumed by the Boeing
(formerly McDonnell Douglas) AH-64 Series Apache attack helicopter.
The AH-1Q anti-armor version was the result
of the Improved Cobra Armament Program (ICAP), to fill the
operational gap left by the failure of the AH-56A Cheyenne program.
The AH-1Q had an M28A1E1 turret, XM65 TOW/Cobra missile subsystem,
infrared sight, and XM128 helmet sight subsystem (HSS). The AH-1Q
was equipped to fire eight Hughes BGM-71 130mm TOW (Tube-Launched,
Optically Tracked, Wire Command-Link Guided) anti-tank missiles
mounted in a pair of two-round pods on the outboard pylons. M200
19-tube 2.75 inch rocket launchers could be carried on the inboard
pylons. The AH-1Q was deployed to Vietnam in 1973, but was unable to
carry a full weapon load in that environment, leading to development
of the AH-1S Cobra. The AH-1Q was the first Cobra to feature the
snub-nosed Telescopic Sight Unit (TSU).
AH-1S Cobra
The AH-1S was a
three-step program to upgrade all AH-1G/AH-1Q/AH-1R Cobras to the
advanced Modernized version. All AH-1S Cobras were redesignated by
the US Army as AH-1P, AH-1E, or AH-1F Modernized Cobras. All
Modernized Cobras, including the AH-1S, AH-1P, and AH-1E used the
M73 reflex sight for optical sighting and fire control and the
Telescopic Sight Unit (TSU). None of the four armament subsystems
used with the four AH-1S variants (Modified, Production, Upgunned,
and Modernized) were interchangeable without considerable
modification or conversion of the AH-1S aircraft.
The designation
"Modified AH-1S" refers to all existing AH-1G/AH-1Q/AH-1R
Cobras modified to Production AH-1S standard beginning in 1976. With
the addition of the XM65 TOW/Cobra missile subsystem the Cobra's
primary mission changed to the anti-tank role, but retained the
direct aerial fire support, armed escort, and reconnaissance
missions. The new armament subsystem was redesignated M28A2. The
Modified AH-1S could be identified by the snub-nosed mounting of the
Telescopic Sight Unit (TSU). The AH-1S also had the traditional
rounded crew canopy, instead of the new semi-flat canopy that became
standard with the new production AH-1S. Some AH-1S Cobras received
the C-NITE upgrade, which allowed the gunner to designate and
acquire targets during night or adverse operating conditions.
First Production
AH-1S (Step 1, 100 aircraft, Mar 77-Sep 78) was the new production
Cobra featuring a new Bell-designed seven-plane semiflat crew
canopy, an improved T-shapped instrument and control panel layout
arranged to enhance nape-of-the-earth (NOE) flight, and new
composite rotor blades. The Production AH-1S was equipped to fire
the XM65 airborne TOW/Cobra anti-tank missile system using the M128
helmet sight subsystem (HSS). The Production AH-1S was equipped with
an upgraded AlliedSignals Engines T53-L-703 1800 shp turbo shaft
engine, gearbox, and transmission that was lacking in the AH-1Q. The
Production AH-1S mounted the new M28A3 armament subsystem with M134
minigun and M129 grenade launcher and retained the 2.75 inch rocket
system. The M28A3 was converted from existing stocks of M28A1
armament subsystems. This new version was first fielded with the
82nd Airborne Division at Fort Bragg, North Carolina in August 1977.
The Production AH-1S could be identified by the new flat panel
canopy.
Upgunned AH-1S (Step
2, 98 new production aircraft, Sep 78-Oct 79), or Enhanced Cobra
Armament System (ECAS) new production Cobra, featured a new
20mm/30mm universal gun turret and retained the M65 TOW/Cobra
missile system. The new M97A1 universal turret was fitted with the
three-barrel M197 20mm automatic gun with automatic compensation for
off-axis gun firing. Since this aircraft lacked the rocket
management system (RMS) it could not use the 2.75 inch rocket system
that was standard on all other model Cobras. The Upgunned AH-1S
could be identified by the tapered tips on the new fiberglass main
rotor blades.
AH-1E Enhanced Cobra
was identical to the Upgunned AH-1S (ECAS), the M65 TOW/Cobra
missile system with the M97A3 armament subsystem. The AH-1E could
use the M130 flare and chaff dispenser. The AH-1E could be
identified by the tapered tips on the fiberglass main rotor blades.
AH-1S Modernized
Cobra (Step 3, 530 aircraft, Nov 79-Jun 81). Of 530 Modernized
Cobras, 387 were converted for old AG-1G Cobras and 143 were from
new Production aircraft. The Modernized Cobra featured a new fire
control system with a pilot's M76 Head-Up Display (HUD), M136 Helmet
Sight Subsystem (HSS), laser rangefinder and tracker, and M26 Fire
Control Computer (FCC). The modernization program also added an M143
Air Data Subsystem (ADS). The installation of the M147 Rocket
Management Subsystem (RMS) permitted use of the standard 2.75 inch
rocket system, in addition to the M65 TOW/Cobra missile system, and
the M197 20mm gun on the new M97A2 universal turret. The Modernized
AH-1S could mount M158 seven-tube, M200 19-tube, M260 seven-tube, or
M261 19-tube rocket launchers. The Modernized AH-1S Cobra had an
infrared jammer mounted on the top of the engine fairing and a hot
metal plus plume infrared suppressor extending from the back of the
engine. The Modernized AH-1S could be identified by the air data
sensor mounted above the right side of the canopy.
AH-1P Production
Cobra was identical to the new Production AH-1S, the M65 TOW/Cobra
missile system with the M28A3 armament subsystem. The AH-1P could
use the M130 flare and chaff dispenser. The AH-1P could be
identified by the flat panel canopy.
AH-1F Cobra
The AH-1F Modernized Cobra is identical to
the AH-1S Modernized Cobra, and can be identified by the air data
sensor mounted above the right side of the canopy. The AH-1F Cobra
is equipped with the Allied Signal Engines (ASE) T53-L-703 1800 shp
turboshaft engine, gearbox, and transmission introduced to the
Production AH-1S Cobra.
Armament consists of the three-barrel M197
20mm automatic gun mounted on the M97A4 armament subsystem. The
Modernized AH-1F is equipped to fire eight TOW (Tube-Launched,
Optically Tracked, Wire Command-Link Guided) anti-tank missiles, and
the Hydra 70 2.75 inch rocket system. It is equipped with the M65
TOW/Cobra missile system, the M147 Rocket Management System with the
M97A4 armament subsystem. The Cobra can also disperse chaff and
infrared jamming flares using the M130 general purpose dispenser.
Some AH-1F Cobras have received the C-NITE upgrade, which allows the
gunner to designate and acquire targets during night or adverse
operating conditions.
AH-1T Cobra
With increasing demands for higher
performance, particularly greater load-carrying capability in high
temperature conditions, Bell developed improved dynamic components
for the Huey series. Application of these components, which included
a larger diameter rotor, led to the 309 attack helo in the early
Seventies. This allowed an increased payload, providing more combat
capability. The subsequent Marine-ordered version of the King Cobra
was designated the AH-1T.
The United States Marine Corps had
identified a need for more armaments; thus, the AH-1T upgrade was
initiated. This aircraft had an extended tailboom and fuselage and
an upgraded transmission and engines. In addition to the
modifications for improved combat effectiveness, major efforts were
made to incorporate the lessons of the Cobra experience in achieving
greater reliability and maintainability. With the TOW missile system
added to its weapons, the AH-1T gave Marines a ground attack
capability far beyond that first envisioned by their predecessors
who took the first Marine Huey Cobras into combat in the late 1960s.
The AH-1T is fully capable of performing
its attack mission in all weather conditions. Additional missions
include direct air support, antitank, armed escort, and air to air
combat. The TOW missile targeting system uses a telescopic sight
unit (traverse 110º, elevation 60º/+30º), a laser augmented
tracking capability, thermal sights and a FLIR to allow for
acquisition, launch, and tracking of all types of TOW missiles in
all weather conditions. The Cobra also uses a digital ballistic
computer, a HUD, Doppler nav, and a low speed air data sensor on the
starboard side for firing, and has in-flight boresighting. External
stores are mounted on underwing external stores points. Each wing
has two hardpoints for a total of four stations. A representative
mix when targeting armor formations would be eight TOW missiles, two
2.75-in rocket pods, and 750x 20-mm rounds. The gun must be centered
before firing underwing stores. Armored cockpit can withstand small
arms fire, and composite blades and tailboom are able withstand
damage from 23-mm cannon hits.small arms fire, and composite blades
and tailboom able to withstand damage from 23-mm cannon hits.
AH-1W Super
Cobra
The AH-1W Super Cobra is a day/night
marginal weather Marine Corps attack helicopter that provides
enroute escort for assault helicopters and their embarked forces. It
is the only western attack helicopter with a proven air-to-air and
anti-radar missile capability. The primary mission of the AH-1W
aircraft is as an armed tactical helicopter capable of helo close
air support, low altitude and high speed flight, target search and
acquisition, reconnaissance by fire, multiple weapons fire support,
troop helicopter support, and point target attack of threatening
armor. The AH-1W provides fire support and fire support coordination
to the landing force during amphibious assaults and subsequent
operations ashore.
The AH-1W is a two-place, tandem-seat,
twin-engine helicopter capable of land- or sea-based operations. The
rear seat pilot is primarily responsible for maneuvering the
aircraft. The front pilot controls the aircraft's weapons systems,
but he also has a full set aircraft controls. The AH-1W
distinguished itself with its more powerful T700-GE-401 fully
marinized engines and advanced electronic weapons capability. The
AH-1W has significantly improved power available in high altitude,
hot environment, and single engine performance. The Super Cobra is
armed with a 20mm turret gun, TOW, Hellfire, Sidewinder, Sidearm
missiles, and 5 inch or 2.75 inch rockets. The HELLFIRE Missile
System increased ordnance delivery and firepower capabilities. The
AH-1W Super Cobra provides full night-fighting capability with the
Night Targeting System (NTS). The Night Targeting System (NTS)
further enhanced the AH-1W's warfighting capability by adding FLIR
sensor, CCD TV sensor, Laser Designator/Rangefinder, Automatic
Target Tracking and FLIR, and CCD TV video recording.
Current AH-1W assets are comprised of a
mixture of new production AH-1Ws and aircraft block upgrade AH-1Ts
remanufactured into the AH-1W aircraft. By the early 1980s, USMC
aircraft inventory was declining due to attrition; a fully navalized
helicopter was sought. In 1983, the USMC contracted with BHI for 44
AH-1Ws. An upgrade to the AT-1T, the AH-1W was received in 1986. The
Tactical Navigation System (TNS) was placed in all production and
block upgrade AH-1W aircraft delivered since February 1991.
Previously delivered AH-1Ws are retrofit with TNS prior to CCM/NTS
induction. The NTS/Canopy/Cockpit Modification (CCM) replaces the
existing canopy, nose faring, and copilot/gunner instrument panel to
make provisions for the NTS and adds the TNS, CDU-800, to the front
cockpit. Additionally, a communication/ navigation upgrade, ECP
1686, incorporated an ARC-210(V)Electronic Protection (EP) Radio, an
ARN-153 V-4 TACAN, and an AN/ASN-163 Global Positioning
System/Inertial Navigation System (EGI) commencing in 1996.
Night Targeting System (NTS) TECHEVAL was
conducted from May through Septempber 1993 by VX-5 at Naval Air
Warfare Center, Weapons Division (NAWC-WD), China Lake; Yuma Proving
Ground, Arizona; White Sands Missile Range, New Mexico; Bridgeport,
California; and on amphibious ships at sea. Follow-on Operational
Test and Evaluation (FOT&E) (OT-IIIA) commenced in February 1994
and concluded in May 1994. NTS OPEVAL was conducted from May through
September 1993 by VX-5 at Naval Air Warfare Center, Weapons Division
(NAWC-WD), China Lake; Yuma Proving Grounds, Arizona; White Sands
Missile Range, New Mexico; Cold Lake, Canada; and on amphibious
ships at sea. Follow-on Operational Test and Evaluation (FOT&E)
commenced during July 1994 and ended in April 1995.
The NTS upgrade provides increased mission,
safety and performance characteristics and incorporates a Canopy/
Cockpit Modification to the front cockpit. The approved OSIPs which
include the ARC-210 (v) EP Radio, the ARN-153V(4)TACAN and the
Global Positioning System/Embedded Inertial Navigation System (EGI)
AN/ASN-163 (V) will also enhance the AH-1W Weapon Systems upon their
incorporation.
The NTS is a modification of the existing
M-65 TOW Missile System that offers a fire control system providing
the flight crew with the ability to detect, acquire, track, lock-on,
range, and designate targets under day, night, and adverse weather
conditions. ECP 1648R4, Canopy/Cockpit Modification is the ECP that
modifies the aircraft to accommodate the NTS. The front cockpit of
the AH-1W has been modified to facilitate the addition of the NTS.
This modification has also resulted in increased efficiency in the
front cockpit and helps divide cockpit workload between the front
and rear cockpits. Specifically, the additions and deletions are:
Expansion of the ASQ-205 Cockpit Control System (CCS) to include the
front cockpit; re-design of the instrument panel to include a more
IFR compatible flight instrument cluster; addition of a 5" x
5" Multi-Function Display (MFD) in the front cockpit; and
addition of the ANVIS HUD system with control heads in both
cockpits. The Night Targeting System (NTS) includes the following
hardware changes to the AH-1W: modification of the M-65 telescopic
sighting unit (TSU) to accomodate the FLIR; an extended Optical
Relay Tube (ORT) to accommodate a CCD TV camera; and a ddition of a
Laser Designator/Rangefinding System (LDRS).
ECP-1674 Electronic Warfare (EW) Suite
reduces aircraft vulnerability with electronic countermeasures. The
suite is designed to alert and protect the aircraft from
surface-to-air and air-to-air missiles. The AN/AAR-47 Missile
Warning System (MWS) provides a visual and aural warning to flight
crews of missile detection, while at the same time the MWS will
initiate countermeasures by sending an eject signal to the AN/ALE-39
Countermeasures Dispenser Set (CDS). The AN/AVR-2 Laser Warning
Receiver detects pulsed laser light (such as a rangefinder) directed
at the helicopter and warns the crew of this activity. It provides
an audio alert and identifies the threat by its type and location
relative to the helicopter. The AN/APR-39A(V)2 Radar Detection
System is a passive omni-directional detection system which receives
and displays information to the pilot concerning the radar
environment surrounding the helicopter.
The AH-1W is operated in eight composite
HMLA squadrons composed of 18 AH-1 and 9 UH-1 aircraft. The AH-1W is
currently being outfitted with a Night Targeting System/Forward
Looking Infrared Radar that provides laser rangefinding/designating
and camera capabilities.
The Marine Corps deployed 4 of 6 active
force squadrons (48 AH-1Ws) to Southwest Asia during Operation
Desert Shield/Desert Storm. The deployment required no additional
augmentation to squadron support personnel and only one Bell
Helicopter technical representative. During Operation Desert Storm,
the AH-1W comprised less than 20% of the attack helicopter force
deployed, yet flew more than 50% of the total attack force
flight-hours. In the entire Desert Shield/ Desert Storm campaign,
SuperCobras flew more than three times the number of hours per
aircraft per month than any other attack helicopter. And during the
"100 Hour War," its reliability and 92% mission readiness
rate were superior to all other attack helicopters by as much as
24%... without any factory-supported maintenance augmentation.
Perhaps most impressive, this record was amassed under some of the
most adverse environmental conditions ever endured in modern
warfare. Temperatures consistently reached the 57-63°C (135-145°F)
range. A mix of fine granite/limestone sand dust the consistency of
talcum powder, was a constant threat to man and machine. And the air
was often filled with a black concoction of burning oil and blowing
sand The final result? Marine Corps crews and their AH-lWs destroyed
97 tanks, 104 armored personnel carriers and vehicles, 16 bunkers
and two antiaircraft artillery sites.
Future Upgrades include provisions for an
Inflatable Body And Head Restraint System (IBAHRS). The IBAHRS
itself will be incorporated upon receipt of the system. An
operational requirement has been identified for a Wing Tip Armament
Station modification and retrofit. Upon approval, this upgrade will
be incorporated into the AH-1W airframe and will include as a
minimum provisions for integration of up to six (6) universal
weapons stations. The Cockpit Integration Requirement identified in
the Operational Requirements Document for the AH-1W Mid Life Upgrade
will be targeted by the 4 Bladed program which is being studied as
another future AH-1W weapon system enhancement.
AH-1Z
UPGRADE PROGRAM
A major upgrade of
the Bell Super Cobra, known as the H-1 Program, is underway. The
program calls for the remanufacture of the US Marine Corps fleet of
180 AH-1W Super Cobra and 100 UH-1N utility helicopters to an
advanced four-bladed configuration. The existing two-bladed
semi-rigid, teetering rotor system is being replaced with a
four-bladed, hinge less, bearing less rotor system. First flight of
the AH-1Z took place in December 2000. The AH-1W entered Low Rate
Initial Production (LRIP) in October 2003. Three AH-1W helicopters
were remanufactured to AH-1Z standard and are in flight testing at
NAS Patuxent River, Maryland. Sea trials in May 2005 included the
first shipboard landing on USS Bataan, Wasp Class amphibious assault
ship. One AH-1Z was delivered to the USMC in October 2005 to begin
Operational Evaluation (OPEVAL) in early 2006. Full-rate production
is scheduled for 2006 with initial operating capability in June
2009. The improvement in flight characteristics provided by the
four-bladed configuration has led to increases in flight envelope,
maximum speed, vertical rate-of-climb, payload and rotor vibration
level.
The Turkish Army
selected the AH-1Z King Cobra in July 2000 with a request for 50 out
of a total requirement for 145 helicopters. In May 2004, it was
announced that the acquisition was to be cancelled. The helicopters
were to be built in Turkey by Tusas Aerospace Industries (TAI).
COCKPIT
Northrop Grumman has
developed the Integrated Avionics Systems for the AH-1Z. The systems
include two mission computers and an automatic flight control system
with four-axis stability control augmentation system. Each crew
station has two 8in x 6in multifunction displays and one 4.2in x
4.2in dual function display, based on active matrix liquid crystal color
technology.
The communications
suite combines the new US Navy RT-1824 integrated radio, UHF/VHF,
COMSEC and modem in a single unit. The navigation suite includes an
Embedded GPS Inertial (EGI), a low airspeed air data subsystem which
allows weapons delivery when hovering and digital map.
In June 2002, Thales
Avionics' TopOwl helmet-mounted display system was chosen for the
USMC AH-1Z. The first system was delivered in January 2003. TopOwl,
also fitted on Tiger, NH90 and Rooivalk helicopters, has integrated
Gen IV image intensifier and FLIR capability and provides transition
from day to night use at the push of a button.
WEAPONS
The Super Cobra can
carry both TOW and Hellfire anti-armor missiles and is being
qualified to carry the Maverick missile. The Raytheon BGM-71 TOW
missile has a range of more than 3km and semi-automatic
command-to-line-of-sight guidance. The AGM-114 Hellfire missile is
manufactured by Lockheed Martin. It is equipped with a semi-active
laser seeker and has a range of 7km. The Super Cobra has
fire-and-forget capability when firing the Hellfire missile in
co-operative mode with laser target illumination.
The Super Cobra was
the first attack helicopter to qualify both the Sidewinder
air-to-air missile and the Sidearm anti-radiation missile. Both
missiles can use the same LAU-7 rail launcher. Sidearm has a range
of more than 15km. AIM-9L Sidewinder is an all-aspect short-range
air-to-air missile produced by Lockheed Martin and Raytheon. The
missile has a range of 15km.
The Super Cobra can
fire the Advanced Precision Kill Weapon System (APKWS), formerly
known as Hydra, family of guided and unguided 70mm rockets or the
larger 127mm Zuni rocket bombs.
The Super Cobra
carries a three-barrel 20mm Gatling gun for close range (up to 2km)
engagement and 750 rounds of ammunition. With the gun in a fixed
forward position, the pilot can aim by maneuvering the helicopter.
Either crew member can slave the turret to the helmet-mounted sight,
and aim the gun by looking at the target.
The AH-1Z for the
USMC will be armed with: 16 Hellfire missiles, six AIM-9 Sidewinder
air-to-air missiles, 70mm rocket pods (7- and 19-shot), as well as
the 20mm gun.
SENSORS
Targeting for the
AH-1W is provided by the Night Targeting System (NTS), jointly
produced by Tamam Division of Israel Aircraft Industries Ltd and
Kollsman. NTS integrates a Forward Looking Infrared (FLIR) which
provides automatic target tracking with a laser designator /
rangefinder and video recorder.
Lockheed Martin is
developing a longer range Target Sight System (TSS) for the AH-1Z to
replace the NTS. TSS includes a third-generation four field-of-view
FLIR based on a 3-5 micron staring array, CCD color TV, eyesafe
laser rangefinder / designator and multi-target autotracker.
Longbow
International (a joint venture of Lockheed Martin and Northrop
Grumman) is developing the Cobra Radar System for the AH-1Z, based
on the Longbow millimeter wave radar on the AH-64D Apache. Cobra is
a pod-based radar that can be mounted on a wingtip or in a stores
position. Cobra can automatically search, detect, classify and prioritize
multiple moving and stationary targets. It has a range of 8km
against moving and 4km against stationary targets.
COUNTERMEASURES
The H1 Super Cobra
upgrade includes provision of a new electronic warfare suite. A new
radar, the AN/APR-39(XE2) from Lockheed Martin replaces the Lockheed
Martin AN/APR-39(V)2 pulse radar and the AEL Industries AN/APR-44
continuous wave radar. The ATK AN/AAR-47 missile warning system has
been included in the upgrade suite. AN/AAR-47 uses infrared
detectors to detect the missile plume. The Goodrich (formerly
Raytheon) AN/AVR-2A laser warning receiver has also been added. The
infrared countermeasures system is the AN/ALQ-144A developed by BAE
Systems IEWS (formerly Sanders, a Lockheed Martin company). The
helicopter is equipped with the AN/ALE-39 chaff and infrared flare
dispenser manufactured by BAE Systems Integrated Defense Solutions
(formerly Tracor) and Lockheed Martin Tactical Defense Systems.
ENGINES
Twin General
Electric T700-GE-401 turboshaft engines provide a total of 2,410kW
or 3,380shp (shaft horsepower). In standard conditions, with an
air-to-air ordnance load the Super Cobra can take off and climb out
at more than 4.1m/sec on only one engine. It can hover Out of Ground
Effect (OGE) at 914m with a load of four TOW and four Hellfire
missiles, full turret ammunition and rockets.
Specifications
|
| Contractor: |
Bell
Helicopter TEXTRON, Inc. (Prime), General Electric, Kollsman
Inc. |
| Power
Plant: |
- Two General Electric T700-GE-401
Turboshaft engines
- Each engine delivers 1,690
horsepower.
|
| Accommodations: |
- Two seats, in tandem (pilot in
rear, copilot/gunner in front)
|
| Performance: |
- Climb rate: 1,925 feet per
minute
- Maximum altitude: 14,750 feet
- Maximum attainable speed: 170
knots (195 mph)
- Maximum cruising speed: 152
knots (173 mph)
|
| Countermeasures: |
- AN/ALE-39 Chaff system and
SUU-4/1 Flare dispensers
|
| Armament: |
- One M197 three barrel 20 mm gun
(mounted under the nose with 750 round ammo container)
- Underwing attachments for four
TOW missiles, eight Hellfire missiles, or one AIM-9L
Sidewinder missile
- Can also be equipped with Zuni
rocket launchers
|
External
Dimensions
| Main
rotor diameter |
14.63
m |
| Main
rotor blade chord |
00.84
m |
| Tail
rotor diameter |
02.97
m |
| Tail
rotor blade chord |
00.305
m |
| Distance
between rotor centers |
08.89
m |
| Wing
span |
03.28
m |
| Wing
aspect ratio |
03.74 |
| Length:
overall, rotors turning |
17.68
m |
| Length:
fuselage |
13.87
m |
| Width
overall |
03.28
m |
| Height
(to top of rotor head) |
04.11
m |
| Overall
height |
04.44
m |
| Ground
clearance, main rotor, turning |
02.74
m |
| Elevator
span |
02.11
m |
| Width
over skids |
02.24
m |
|
Areas
| Main
rotor blades (each) |
006.13
m2 |
| Tail
rotor blades (each) |
000.45
m2 |
| Main
rotor disc |
168.11
m2 |
| Tail
rotor disc |
006.94
m2 |
| Vertical
fin |
002.01
m2 |
| Horizontal
tail surfaces |
001.41
m2 |
|
|
Weights
and Loadings
| Weight
empty |
004.634
kg |
| Mission
fuel load (usable) |
946
kg |
| Maximum
useful load (fuel and disposable ordinance) |
002.065
kg |
| Maximum
Takeoff and landing weight |
006.690
kg |
| Maximum
disc loading |
039.80
kg/m2 |
| Maximum
power loading |
004.42
kg/kW |
|
Performance
(At Maximum T-O weight, ISA)
| Never
exceed speed (Vne) |
190
knots |
| Maximum
level speed at S/L |
152
knots |
| Rate
of climb at S/L, OEI |
244
m/minute |
| Service
ceiling |
More
than 4,720 m |
| Service
ceiling, OEI |
More
than 3,660 m |
| Hovering
ceiling |
- IGE
|
4,
495 m |
- OGE
|
915
m |
| Range
at S/L with standard fuel, no reserves |
317
nm |
|
|