От	Олег Радько
К	All
Дата	23.11.2002 22:28:26
Рубрики	Флот;

2 apple16

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Добрый день!
Хотел Вас спросить, нет ли чего в вашем janes по ПЛУР ASROC и IKARA, а также ПКР Sea Skua, AS.34 Kormoran 1/2 и Gabriel...
С уважением.

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От	Олег Радько
К	Олег Радько (23.11.2002 22:28:26)
Дата	25.11.2002 17:50:46

Ocмелюсь попросить еще

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Harpoon, Excocet и Rb-08 (была такая шведская).
С уважением.

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От	apple16
К	Олег Радько (25.11.2002 17:50:46)
Дата	26.11.2002 15:19:39

Harpoon из старых запасов (попозжее остальное) - фотки видно?

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SURFACE-TO-SURFACE MISSILES, UNITED STATES OF AMERICA
Date Posted: 28 January 2002
Jane's Naval Weapon Systems 02
RGM-84/UGM-84 HARPOON (GWS 60)
Type
Medium-range anti-ship missile.
Development
The most widely used, western ship-launched anti-ship missile began life as a requirement for an air-launched anti-surface weapon
as part of the Lockheed P-3C Orion step improvement programme. The new weapon was required by the US Navy but McDonnell
Douglas (now Boeing Company, Military Aircraft & Missile Systems Group) had been conducting private studies since 1965 for a
similar requirement. This was modified as a result of the sinking of the Israeli destroyer Eilat by Styx (qv) missiles in 1967.
Following this event the US Navy expanded the requirement into a multiplatform missile including surface ships and submarines.
An official request for proposals was issued in January 1971 and seven months later McDonnell Douglas won a development
contract for a missile given the name Harpoon, which had been previously proposed for an air-launched anti-submarine weapon
designed for use against surfaced `Juliett' and `Echo' class missile-carrying submarines. In May 1973, the US Navy selected the
Harpoon as its prime anti-ship missile from aircraft (AGM-84A), submarines (UGM-84A) and surface warships (RGM-84A); the
first foreign order, from Turkey, was placed later in that year although weapons were not delivered until 1977. The first guided
weapon flew successfully in December 1972 and operational testing was completed in June 1978, the ship-launched version
showing a 100 per cent success rate. Pilot production began in 1975 and the missile entered service in 1977 with the US Navy in the
`Belknap' class cruiser USS Sterret (CG 31). The UGM-84 became operational in 1981 and about 1,000 were delivered to the US
Navy whose last Harpoon 'Block I' was received in 1991. In the late 1990s, the US Navy began to withdraw UGM-84 from its
inventory and this process was completed in 1997. The Royal Navy will withdraw its weapons from 2003, although there are plans
to acquire Harpoon Block II for the 'Astute' class.
The initial production version Block 1, sometimes referred to as Block 1A, was followed by the sea-skimming guidance version
for the Royal Navy which became RGM-84B, although the UK designation for the system was GWS 60. This capability was
introduced into the Block 1B (RGM-84C) which entered service in June 1982. Already, a further development capable of indirect
attack, with greater range and improved electronics including better ECCM performance and tactical options was under
development. This entered production in 1984 as the Block 1C (RGM-84D) while in September 1989 McDonnell Douglas received
a US$9.8 million contract to develop an extended-range missile with re-attack capability as the Block 1D (RGM-84F). The missile
was originally scheduled to enter service about 1992 and the first test flight, in an air-launched configuration, was made at the
Pacific Missile Test Center, Point Magu, California in late September 1991 but, with the end of the Cold War, development was
abandoned. In 1996, the company revealed plans for an improved Block 1D which had the provisional designation Harpoon P3I
which became Block 1G which entered service in 1997 and is now the prime export model. An Aerospatiale survey of anti-ship
missile market share in June 1993 stated that Harpoon possessed 43 per cent of the Western manufacturers' share of the world
market. In November 1997, Boeing (who took over McDonnell Douglas in 1997) revealed it intended to produce these missiles in a
commercial manner so they could be purchased off the production line rather than building them to specific orders.
The Harpoon missile designation system is confusing because the missile is often referred to by two designations. The Block
number refers to the mid-course guidance programme while the RGM/UGM (AGM for air-launched weapons) refers to the model
of missile. The full list is as follows:
Block Model
1 AGM/RGM/UGM-84A
1 UGM-84B (Royal Navy version of Block
1)
1B AGM/RGM/UGM-84C
1C AGM/RGM/UGM-84D
1D RGM-84F
1E AGM-84E (SLAM)
1G AGM/RGM/UGM-84G
SLAM-ER AGM-84H
1J Proposed for Harpoon 2000 (now Block
2)
2 AGM/RGM/UGM-84L

Note: A/B/C/D-1 missiles are launched from ASROC
ships.
A/B/C/D-2 missiles are launched from Tartar ships.
A/B/C/D-3 missiles are launched from smaller warships
and Mark 140 launcher systems.
C-4 missiles are launched from UK containers.
A/B/C/D-5 missiles are launched from Mark 141 launcher
systems installed in larger warships.
There was no Block 1F.
By 1994, there were few of the original Block 1A missiles still in service although in mid-1991 McDonnell Douglas was awarded
a contract to upgrade such missiles to Block 1A(v) standard for US and foreign forces. Most of the remaining Block 1 missiles have
been upgraded to Block 1B standard and McDonnell Douglas anticipated upgrading up to 2,000 missiles (that is some 28 per cent)
to RGM/UGM-84G standard. In January 1992, Harpoon was capable of use in 189 US and 207 allied surface ships, 76 US and 49
allied submarines, 1,211 US (including 30 B-52G of the USAF) and 368 allied aircraft. Other platforms have the complete Harpoon
support and test facility package but weapons are not normally installed. It is interesting to note that Harpoons (Block 1C) from the
decommissioned `Peder Skram' class frigates have been adapted by NEA Lindberg for coast-defence purposes in order to meet a
Danish requirement.
The missile's average flight reliability of 93.35 per cent is shown grouped by fiscal year procurement:
FY Missiles Successes %
Launched
75-76 98 87 88.77
77-78 73 68 93.15
79-81 114 106 92.98
82-89 136 134 98.5
Total 421 395 93.35
The missile has seen operational service in the Persian Gulf and is believed to have been involved in the sinking of a number of
Iraqi ships, and possibly some tankers. In an engagement fought between the US Navy and Libyan naval forces in the Gulf of Sidra
on 24-25 March 1986, five Harpoons fired from aircraft and by the cruiser USS Yorktown (CG 48) sank the corvette Ean Zaquit and
fast attack craft Waheed and severely damaged the corvette Ean Mara together with one of the Waheed's sister ships. In an
engagement between American and Iranian warships in the Persian Gulf on 18 April 1988, four air- and surface-launched Harpoons
sank the Iranian frigate Sahand and the fast attack craft Joshan. The only use of Harpoon during Operation 'Desert Storm' was by
the Royal Saudi Navy which claimed an Iraqi minelayer on 24 January 1991.
To provide a conventionally tipped, precision-attack, air-launched weapon, McDonnell Douglas developed SLAM (Standoff
Land Attack Missile) during the late 1980s. The first production missile AGM-84E was delivered to the US Navy in November
1988. A version of this missile for shipborne use was test fired from the `Ticonderoga' (CG 47) class cruiser USS Lake Champlain
(CG 57) on 26 June 1990 at the Pacific Missile Test Range, Point Magu, California. The firing was to demonstrate the capability as
part of a US Navy test and evaluation programme to decide whether or not a ship-launched SLAM would be of operational value.
Further trials were carried out between 1995 and April 1996.
In February 1995, McDonnell Douglas received a US$3 million contract for another two ship-launched SLAM demonstrations in
support of the Surface Fire Support programme. The demonstration involves two missiles controlled by an SH-60B helicopter and
an F/A-18 strike aircraft. Seven air-launched SLAMs were used during Operation 'Desert Storm' against Iraqi targets and, in 1994,
development began of an extended-range version of the SLAM, known as SLAM Expanded Response (SLAM-ER) or AGM-84H,
as a private venture proposal for retrofitting into existing SLAMs. An air-launched weapon successfully completed operational test
and evaluation on 6 March 2000 and full-rate production was authorised in May with existing missile stocks being retrofitted to
meet a requirement for 700 rounds. In April 2001, it was revealed that the US Navy was considering a ship-launched version of
SLAM-ER as a stop-gap solution to a requirement to striking targets of opportunity. Israeli Harpoons have reportedly already had a
data-link system upgrade.
At the US Navy League in April 1996, McDonnell Douglas revealed plans to produce Harpoon 2000 (also called Harpoon 1J), a
joint venture with the US Navy's Cruise Missiles and Joint Unmanned Aerial Vehicles Program Office. The new missile, later
designated Harpoon Block 2 or Block II, evolved into a dual-role weapon primarily for anti-shipping requirements but with a
limited land-attack capability.
Early in 1998, the company was negotiating with the US Defense Department to secure finance for development in FY98 and
later the production of kits for retrofitting into missiles for the US Navy. However, the US Navy has become more interested in
land-attack capability for surface-to-surface missiles withdrawing the UGM-84 Sub Harpoon from submarines from 1996 and
displaying little interest in anti-ship missiles for its future surface combatants and, consequently, is unlikely to upgrade its weapons
to Block II standard to the focus of the marketing effort was upon export markets with Denmark the launch customer. The Royal
Navy is considering acquiring Block II for the 'Astute' class submarines.
The first flight of Block II was anticipated in May 2001 with three tests by July and initial operating capability in the first quarter
of 2002, and in the third quarter of 2000 Boeing stated that at least seven navies had modified ships to accept Block II missiles.
Early in 1998, McDonnell Douglas anticipated total orders of 950 retrofit missiles from the US Defense Department and from
international customers 1,500 retrofits (from the New Year of 2002) and 1,100 new-build missiles (from early 2002). In late-1998
Boeing stated it was considering a Block III weapon which would probably begin development circa 2003. This was later
redesignated as Block II Plus, but it is unclear whether any progress will be made.
Late in 2000 it was revealed the US Navy is considering an extended range version of Harpoon using SLAM-ER technology. The
US Navy is also re-considering anti-ship requirements for its Harpoon, Boeing having offered Block II upgrade to their inventory.
In May 2001, the US Navy tested a Block II missile from the USS Decatur (DDG-73) with further tests in the autumn. The Block II
missile will also be offered for the land-attack requirement against SM-4 (qv), NTACMS (qv) and Tomahawk (qv).
Description
The Harpoon missile is a slim cylinder with pointed nose and cruciform wing/fin configuration. Both the wings and fins are of
cropped delta planform with the former being broad while the latter are narrow. Air-launched Harpoon and those ship-launched
from ASROC launchers have fixed wings but the remainder have wings that are on streamlined hinges just above the wing roots.
Between the lower pair of wings is a flush air intake. To adapt the missile for use from various launchers, the arrangements of
`shoes' which hold the missile to the launcher differ depending upon the launchers. Internally the Harpoon is divided into guidance,
warhead, propulsion and control sections and an integral booster.
The guidance compartment has the Texas Instruments (now Raytheon TI Systems Inc) PR-53/DSQ-28 J-band (10 to 20 GHz)
two-axis active radar seeker with flat, phased-array antenna which may be rotated 90º. Behind it is the missile midcourse guidance
unit which includes a Lear Siegler three-axis attitude reference platform and an IBM 4PiSP-OA 16-bit digital computer which acts
as the autopilot. The Honeywell or Kollsman AN/APN-194 radar altimeter has a transmitter antenna in this compartment and a
receiver antenna in the warhead compartment. The Block 1B system, introduced in 1982, featured improved ECCM performance
while in the Block 1C, introduced in 1985, there were a number of improvements to the range, fuze and seeker. The sea-skimming
performance was improved, the missile was capable of an indirect approach to the target by means of way points and the seeker had
enhanced ECCM performance.
The 221.6 kg semi-armour-piercing warhead with 100 kg of explosive has a contact delay fuze and is produced by the China
Lake Naval Weapons Center. The propulsion compartment contains a tank with some 45 kg of kerosene-based fuel (JP6 in Block
1/1B and JP10 in Block 1C/D), the air intake and the pyrotechnically initiated Teledyne CAE J402-CA-4000 single-spool turbojet,
with combined axial/centripetal compressor, which gives a maximum thrust of 2.92 kN and an endurance of 15 minutes. Behind it is
the electrical actuation system and the Thiokol or Aerojet 137 kg booster. The booster provides some 5,400 kg of thrust for about
2.9 seconds.
The missile may be fired from the Mark 11/13 (qv) (used with Tartar or Standard) or the Mark 112 (ASROC) launcher. There are
two dedicated launcher systems; the Mark 140 Mod 0 for fast attack craft and corvettes and the Mark 141 Mod 1 for larger
warships. The Mark 141 features shock-resistant and thick-wall assemblies, which are usually used in larger vessels. Each has a
support structure while the front ends of the launcher tubes are held by a clamp frame assembly. The central and rear ends are held
by stacking frames with the thick wall assemblies providing armour protection for the missiles against fragments. The Mark 140
features aluminium launcher containers designed for 15 firing refurbishment cycles. These containers are held together and to the
aluminium support structure by stacking frames. Both can launch missiles at the rate of one every 2 seconds but, with four
launcher-containers, the Mark 140 weighs 4.02 tonnes while the Mark 141 weighs 5.9 tonnes. Usually ships carry a pair of launcher
systems.
The launcher-containers are inclined at an angle of 35º while the launcher systems either face forwards, but offset from the
centreline, or are at 90º to the centreline facing starboard and port. The Mark 140 system is 4.65 m long, 1.38 m wide and 3.85 m
high and requires 6.42 m 2 . However, with the development of indirect attack versions using `dog leg' flights (Block 1 C/D), the
launchers can now face any direction. Normally launcher systems have four launcher-containers but twin-container configurations
are used by the Iranian, the Israeli (Mark 140) and Pakistani (Mark 141) navies and these weigh 2.15 tonnes. The missiles were
originally removed from the launcher-container annually for inspection but may now be left for four years with surface-launched
weapons and five years for submarine-launched weapons.
Alternative launchers to the Mark 141 are being considered including a low-signature canister which might be incorporated into a
ship's superstructure. Consideration continues to be given to a vertically-launched weapon for use with the Mark 41 (qv) launcher
system.
Submarine-launched weapons are in special, unpowered, buoyant capsules all of which are now manufactured by Lucas
Aerospace, although some earlier capsules were built by McDonnell Douglas in St Louis. These consist of a nose cap, the main
body and the aft body. The nose cap consists of a broach pressure sensor, explosive bolts and a nose removal rocket. The main body
is a tube with shock isolation rails which also guide the missile out during the exit phase. The missile is fitted with a sabot assembly
at the nose to provide further support and shock protection. The sabot straps are cut and the sabot falls away during the exit phase.
The aft body mates with the rear of the missile by means of pyrotechnic bolts and consists of a folding control fin and planes. It
links the capsule system sequencing controls to the submarine through an umbilical cord. Each submarine carries six to eight
missiles, depending upon class.
The ship fit also includes the McDonnell Douglas AN/SWG-1A (V) weapon control system. This consists of the weapon control
console with a data system cabinet and a weapon-control and indicator panel. There is also a data processor and a data conversion
unit, the launcher switching unit and launcher relay assemblies. On the bridge there is an engagement course indicator which shows
ship heading, target bearing and the weapon coverage for each launcher. This consists of the weapon-control console with a data
system cabinet which is 130 cm high and 46 × 80 cm and a weapon control and indicator panel which is 42 × 54 cm. These two may
be separated in ships with smaller CICs. Within the data system cabinet is a data processor with data conversion unit, built-in test
circuits and power supplies. Ships also use the Harpoon data processor which interfaces with the data conversion unit and the
missile to monitor target data which it periodically converts into location data as the basis for fire-control calculations. It also
controls the launch sequence. The weapon control console has launcher switching units which link with the launcher relay
assemblies on each launcher support structure. On the bridge is an engagement course indicator which shows the ship heading,
target bearing and weapon coverage for each launcher.
In submarines, most export submarines and US vessels with Mark 113 fire-control systems have a separate Harpoon console and
data processor known as the Encapsulated Harpoon Command and Launch System (EHCLS), but in Mark 117 the Harpoon
fire-control system was integrated (see Mark 113/117/118 command and weapon control systems entry). The EHCLS weapon
control unit is subdivided into two 10 × 30 cm sections; the data unit and the control panel, which together select the operating and
attack modes as well as monitoring tube status, with target data entered manually. The Harpoon data processor, junction box, power
conversion unit and simulator/test set are in the weapon compartment.
Data is received from ship sensors and processed by the fire-control system. This is then transmitted to the SWG-1A which
activates the missile, selects the flight pattern and seeker search modes (with small, medium or large acquisition `windows') as well
as providing target range and bearing data for a range and bearing launch. Alternatively there can be a bearing only launch in which
the missile is aimed along the target bearing. Here the seeker is activated early to scan a 90º sector. If no target is acquired after a
suitable time, the missile resorts to a preset search pattern. By 1998, the standard of SWG-1A was (V) 8/9 with enhanced data
processing, faster displays, shoreline display, an obstruction database and improved interfaces. The (V) 9/10 for Block 1G entered
service in 1999 with further enhancements to the processor and software which includes automatic shoreline avoidance, eight
waypoints and a downloadable obstruction database. The (V) 10/11 system is compatible with Harpoon Block 2/II, which will be
capable of multiple target engagement, improved littoral performance and GPS initialisation.
The missile is launched and the booster carries it to an altitude of 430 m where the turbojet is activated and the booster is
jettisoned. The missile may be launched to engage targets at 180º to the platform's course and up to four may be launched
simultaneously. The Block 1C may be launched up to 80º off axis.
The Encapsulated Harpoon Weapon System (EHWS) receives target data manually or automatically through the ship fire-control
system. The operator selects both the seeker search pattern mode and the source for target data allowing the seeker to select one of
three search modes. The capsule is then ejected from the torpedo tube at a velocity of some 15.25 m/s and once it is clear both the
fin and the planes deploy.
Initially the planes assist buoyancy movement, the angle depending upon the angle of the torpedo tubes, but when the optimum
glide angle of 45º is reached they neutralise this movement. When the broach sensor recognises the capsule is near the surface it
initiates the sequence in which both the nose cap and the aft body are jettisoned and the booster is ignited. The booster burns for 3
seconds and takes the missile out of the water to near cruise velocity at which point the turbojet operates. The missile then operates
in the same way as air- and surface-launched Harpoon.
In the Block 1 and Block 1B the missile then descends to its cruising altitude and at a point preset by the launch platform,
activates its seeker to acquire and designate the target. The Harpoon can fly one of three fixed (large, medium and small) or one
variable search patterns. In the terminal phase the Block 1 missiles would then climb suddenly at a distance of about 1.0 n miles (1.8
km) from the target to make a 30º dive attack upon the target. The seeker is believed to optimise the horizontal radar cross-section
but is adjustable. In both systems this terminal phase is an option and sea-skimming is the other option.
The Block 1C has a similar performance to the Block 1B but has a number of additional options. It can fly at relatively high
altitude for the first part of its path to avoid friendly ships or intervening low landmasses, and it can approach the target indirectly
by means of a preselected waypoint, the missile being capable of up to three waypoint course changes with turns greater than 15º,
although UGM-84 (and AGM-84) generally have only one waypoint. Approaching the target it can use selectable seeker search
expansion patterns and for the terminal phase it has the alternatives of a sea-skimming approach or a low-apogee `pop-up'
trajectory. There are reports that Israeli missiles have a datalink system for updating targeting data.
The Block 1D missile is only for air and surface ship launch. It is 65 cm longer through the addition of a larger fuel tank with 32
kg of fuel. Wing slot covers were to be added, the battery replaced and the missile guidance unit modified. The missile would have
had a 75 per cent increase in range but the initial search would have been delayed. When the target was acquired the missile would
descend to sea-skimming altitude earlier and strike the target 30 to 60 cm lower down than earlier missiles which, with the extra
fuel, would have increased the damage inflicted. In the event of the target being lost the missile would undertake a clover leaf-like
search pattern until it re-acquired the target. Sea-skimming and high-angle dive attacks were also available.
The Block 1G is for ships and submarines whose lightweight launcher-containers are too small for Block 1D. The upgrading
involves incorporating the Block 1D re-attack logic and lower impact point capability by means of changing the memory and fast
CPU cards in the mid-course guidance unit. The changes can be performed in country and no alterations to the SWG-1A are
necessary. Like earlier missiles it is capable of three way-point turns.
SLAM is a conventional Harpoon missile but with the seeker replaced by a Hughes imaging infra-red seeker, a datalink and a
multichannel Rockwell-Collins Global Positioning System (GPS). The seeker is identical to that used in the Maverick air-to-surface
missile while the datalink is the same as that used in the Walleye `smart' bomb system. The GPS system includes a navigation
processor, and a Mark 82 interface so the missile remains compatible with the SWG-1A weapon control system. The missile's
mid-course guidance unit has minor hardware and software modifications. The missile is 65 cm longer and 90.72 kg heavier than a
conventional Harpoon. A longer-ranged SLAM incorporating a new seeker head and the wing unit of Tomahawk was unveiled in
1994 as SLAM-ER.
The missile is launched from a launcher system and is then supported by an aircraft. In the test this aircraft was a LAMPS III
(Light Airborne MultiPurpose System Mk III) helicopter (Sikorsky SH-60B Seahawk). During the cruising phase the autopilot is
updated through the GPS receiver/processor to ensure the seeker is pointed directly towards the target, a facility which is especially
useful as the missile is also capable of multiple way points. The seeker is activated during the last 60 seconds of the terminal phase
and sends a video image through the datalink to the aircraft, the crew of which selects a specific aiming point on the target and lock
the seeker on to it. In the event of a target of opportunity being discovered by the aircraft, a short-range engagement involving
launch-on-bearing is undertaken in which the missile does not use GPS but relies exclusively upon the datalink and seeker. In
August 1996, the SLAM automated mission planning system entered service with the US Navy. Sea SLAM is envisaged as carrying
a variety of warheads including unitary and sub-munition with the latter potentially including eight Brilliant anti-armour and 153
Combined Effects Bomblets.
Israeli Harpoons have reportedly received a datalink upgrade. Tadiran Spectralink indicated that their Guided Weapon Data Link
(GWDL) operating in UHF (300 MHz-1 GHz), L (1-2 GHz), S (2-4 GHz), C (4-8 GHz), X (8-12 GHz) and Ku-Ka (12-40 GHz)
bands with TDMA protocol security for both up-links and down-links is used with this missile. The data/video rates are 1.5, 2, 3 or
6 Mbps and a helicopter is used as the forward observing, relay and attack platform.
Harpoon Block II will be offered as both new build and as an upgrade package (at 20 to 30 per cent of the cost of a new missile)
and has been designed specifically to provide improved performance in littoral waters from surface combatants or submarines.
Externally it is similar to earlier weapons but internally there are improvements to the seeker, guidance section and warhead. The
seeker now features surface-mounted technology with all digital processing using only five printed circuit boards, a VME data bus
and the two one-axis gyros replaced by a single two-axis unit. The improvements will make it possible to adjust the radar seeker's
search pattern to reduce land clutter effects as well as offering other functions including Doppler processing for a
coherent-on-receive function. In the guidance section the midcourse guidance unit is replaced with a guidance control unit which
incorporates the Honeywell HG 1700 ring laser gyro-inertial measurement unit (used in the Joint Direct Attack Munition or JDM)
the mission computer based upon Motorola 68040 processors and Collins GEM III Global Positioning System Global Positioning
System (GPS) receiver used in SLAM-ER. The warhead features insensitive explosives with a new fuze providing detonation either
upon impact or delayed.
While AN/SWG-1A (V) 10/11 will be compatible with Harpoon Block II, Boeing is developing an Advanced Harpoon Weapon
Control System for use by surface ships, submarines and coastal defence systems. It would use COTS technology based such as
Unix operating system, X Windows/MOTIF graphics and Ada and C++ language software, housed in multifunction consoles or a
stand-alone display compatible with digital local area networks and in addition to being interfaced with the ship GPS would have
RS-232 or RS-422 standard interfaces. It would provide simplified missile engagement planning with multi-automatic waypoints
allowing the missile or missiles to avoid land or friendly ships while third-party targeting data can also be incorporated.
The missile and control features permit conventional, 'blue water' anti-ship operations but in littoral waters allow for OTH
targeting by helicopter to select targets concealed among merchant shipping or close to land, to attack ships in port or even to strike
land targets. For littoral ASuW against targets close to land the missile would receive shoreline data before launch and during the
mid-course flight would use GPS guidance while in the terminal phase the seeker would 'blank' land returns to acquire the target.
For attacks upon targets in port or on land the missile would be launched and make the usual low-level approach but would place
greater reliance on the GPS/inertial navigation system to avoid land or ships in a course which can incorporate up to eight
waypoints. As it approaches the coast would climb to a pre-selected vertical waypoint, select the fuze delay and impact angle then
approach the target area using inertial guidance. In the terminal phase it would climb and then dive with a CEP of 10/13 m.
A Block II Plus version is being considered which might add an infra-red seeker to the radar element which might also provide
automatic target recognition, track-while-scan operation and automatic target acquisition. New warhead options are being
considered and an 18 in (45 cm) extension devised (but never incorporated) for Block 1D might be added to increase range. It is
unclear whether or not vertical launch is being considered, although this was proposed for Block III, and Lockheed Martin has
shown artist's impressions of canisters for vertically launched Harpoon/SLAM-ER which could be used with the GMVLS Mark 41
(qv). A ballistic trial of a vertically-launched Harpoon was conducted during development of GMVLS Mark 41 (qv).
Operational status
Some 7,800 missiles had been ordered delivered, nearly 4,000 to export customers with some 17 per cent of these missiles being
Sub-Harpoon. Deliveries to the US Navy ceased in 1992 but upgrade programmes will continue until 2015. Blocks 1B, 1C, 1D and
II are the only missiles currently in production. Harpoon is installed in, or has been selected for the following ships:
Country Class/Ship Type Missile Launcher Associated
Radar
Australia `Collins' SSK UGM-84C TT -
'Anzac' (MEKO
200)
FF RGM-84A/C * Mk 13 9LV 453
'Oliver Hazard
Perry'
(`Adelaide')
FF RGM-84C Mk 13 SPS-55
Bahrain 'Oliver Hazard
Perry'
FF RGM-84C Mk 13 SPS-55
Canada `Halifax' FF RGM-84C/D Mk 141 Sea Giraffe 150
Denmark `Niels Juel' FF RGM-84C Mk 141 9GR600
'Flyvefisken' PB RGM-84C/L Mk 141 Scanter
Egypt 'Romeo' SSK UGM-84C TT -
`Descubierta' FF RGM-84C Mk 141 DA 05
'Oliver Hazard
Perry'
FF RGM-84C Mk 13 SPS-55
`Knox' FF RGM-84C Mk 112 SPS-67
Germany `Lütjens' DD RGM-84A/C Mk 13 SPS-10
`Bremen' FF RGM-84C Mk 141 DA 08
'Sachsen' FF RGM-84F Mk 141 APAR
Greece Type 209/1100 SSK UGM-84C TT -
Type 214 SSK UGM-84C TT -
`Charles F
Adams' ('Kimon')
DD RGM-84A/C Mk 13 SPS-10
`Knox' ('Epirus') FF RGM-84A/C Mk 112 SPS-10/67
MEKO 200
('Hydra')
FF RGM-84G Mk 141 MW 08
'Kortenaer' FF RGM-84A/C Mk 141 ZW 06
'Pirpolitis/Mod
Pirpolitis'*
FAC RGM-84C Mk 140 Triton
`Osprey 55'
('Armatolos')*
FAC RGM-84A/C Mk 140 Triton
Indonesia `Van Speijk' FF RGM-84A Mk 141 DA 05
Iran 1 'Combattante II' FAC RGM-84A Mk 140 WM 28
Israel 2 `Dolphin' SSK UGM-84C TT -
`Eilat' FC RGM-84C Mk 140 SPS-55
`Aliya/Hertz'
(Saar 4, 5)
FAC RGM-84C Mk 140 Neptune
`Reshef' (Saar 4) FAC RGM-84C Mk 140 Neptune
Japan 3 `Oyashio' SSK UGM-84C TT -
`Harushio' SSK UGM-84C TT -
`Yuushio' SSK UGM-84C TT -
`Kongou' DD RGM-84C Mk 141 OPS 28
`Hatakaze' DD RGM-84C Mk 141 OPS 28
'Improved
Murasame'
DD RGM-84C Mk 141 OPS 28
`Asagiri' DD RGM-84C Mk 141 OPS 28
'Murasame' DD RGM-84C Mk 141 OPS 28
`Hatsuyuki' DD RGM-84C Mk 141 OPS 18
`Tachikaze' DD RGM-84C Mk 13 OPS 16/28
`Takatsuki' DD RGM-84C Mk 141 OPS 17
`Abukuma' FF RGM-84C Mk 141 OPS 28
`Yubari' FF RGM-84C Mk 141 OPS 28
Ishikari FF RGM-84C Mk 141 OPS 28
Korea, South 'Gearing' DD RGM-84C Mk 141 SPS-10
KDX-2 FF RGM-84C Mk 141 MW 08
`Okpo' FF RGM-84C Mk 141 AWS-6A
`Ulsan' FF RGM-84C Mk 141 ZW 06
`PSMM 5' FAC RGM-84A Mk 140 HC 75
Netherlands `Walrus' SSK UGM-84C* TT -
'De Zeven
Provincien'
DD RGM-84F Mk 141 APAR
`Jacob van
Heemskerck'
FF RGM-84C Mk 141 ZW 06
`Kortenaer' FF RGM-84A/C Mk 141 ZW 06
`Karel Doorman' FF RGM-84A/C Mk 141 ZW 06
Pakistan 4 `Agosta' SSK UGM-84A TT -
`Daphne' SSK UGM-84A TT -
`Amazon' (Type
21)
FF RGM-84D Mk 141 Type 992
Portugal MEKO 200
(`Vasco da Gama'
)
FF RGM-84C Mk 141 MW 08
Saudi Arabia `Badr' FC RGM-84C Mk 140 SPS-55
`Al Siddiq' FAC RGM-84C Mk 140 SPS-55
Singapore `Victory' FC RGM-84C Mk 140 ZW 06
`Lürssen FPB 45'
('Sea Wolf')
FAC RGM-84C Mk 140 WM 28
Spain 5 'Álvaro de Bazán' DD RGM-84F Mk 141 SPS-67
'Oliver Hazard
Perry' (`Santa
Maria')
FF RGM-84C Mk 141 SPS-64
'Descubierta' FF RGM-84A/C Mk 141 SPS-10
`Baleares' FF RGM-84C Mk 141 SPS-10
Taiwan `Knox' FF RGM-84A Mk 112 SPS-10/67
Thailand `Naresuan' FF RGM-84A Mk 141 SPS-64
`Knox' FF RGM-84C Mk 112 SPS-10/67
`Rattanakosin' FC RGM-84A Mk 140 ZW 06
Turkey Type 209/1400 SSK UGM-84C TT -
'Oliver Hazard
Perry'
FF RGM-84C Mk 141 SPS-55
`Knox' FF RGM-84C Mk 112 SPS-10/67
MEKO 200
(`Yavuz/Barbaros'
)
FF RGM-84C Mk 141 AWS 6
'Yildiz' FAC RGM-84C Mk 140 AWS-6
'Kiliç' FAC RGM-84C Mk 141 MW08
`Dogan' FAC RGM-84A Mk 140 WM 28
UAE 'Kortenaer' FF RGM-84G* Mk 141 Scout
UK 6 `Trafalgar' SSN UGM-84D TT -
'Astute' SSN UGM-84D TT -
`Swiftsure' SSN UGM-84D TT -
'Daring' (Type
45)
DD RGM-84 * Mk 141 S1850
`Duke' FF RGM-84C Mk 141 Type 996
'Broadsword'
Batch 3
FF RGM-84C Mk 141 Type 967/968
USA 7 `Sturgeon' (SSN
637)
SSN UGM-84C* TT -
`Los Angeles'
(SSN 688)
SSN UGM-84C* TT -
`Ticonderoga'
(CG 47)
CG RGM-84D/F Mk 141 SPS-55
`Arleigh Burke'
Flight I (DDG 51)
DD RGM-84D/F Mk 141 SPS-67
`Arleigh Burke'
Flight II (DDG
72)
DD RGM-84D/F* Mk 141 SPS-67
'Arleigh Burke'
Flight IIA (DDG
79)
DD RGM-84D/F* Mk 141 SPS-67
`Oliver Hazard
Perry' (FFG 7)
FF RGM-84 D/F Mk 13 SPS-55

Notes:
In submarine entries TT stands for Torpedo Tube and radars are not shown because submarines use sonar for fire
control. Most surface warships operate with only half their potential number of Harpoons.
*Ships equipped to carry Harpoon but no weapons embarked.
1 Most of the 'Combattante II' class have C-802 missiles. It is unlikely that there are more than six RGM-84A
remaining in the Iranian inventory.
2 The Israeli Saar 4.5 ('Hetz' and 'Aliya' classes) and Saar 4 ('Reshef' class) FACs carry a mixture of Harpoon and
Gabriel missiles.
3 The 'Improved Murasame' and 'Murasame' may carry Harpoon but usually have Japanese SSM-1B missiles
embarked.
4 In the Pakistan 'Amazon' class only PNS Shahjahan, Badr and Babur carry Harpoon.
5 The Spanish 'Álvaro de Bazán' class may receive Block II.
6 The Royal Navy plans to withdraw Sub-Harpoon from its inventory between 2003 and 2005. However, Block II
might be acquired for the 'Astute' class. The 'Daring' Batch 1 will be fitted for, but not with, Harpoon. The 'Duke'
class normally embark only four launchers.
7 Harpoon is not always carried by 'Ticonderoga' class cruisers or the 'Arleigh Burke' Flight II/IIA destroyers.
Specifications
Block 1/1C
Length with booster: 4.63 m
Length without booster: 3.84 m
Diameter: 0.34 m
Wing span: 0.83 m
Weight with booster: 681.9 kg
Weight without booster: 519.3 kg
Max speed: M0.85
Range: 50 n miles (92 km) (1A/B); 67 n miles (124 km) (1C)
Warhead: 221.6 kg
Guidance: Inertial and active radar
Block 1D/Sea SLAM
Length with booster: 5.23 m
Length without booster: 4.4 m
Diameter: 0.34 m
Wing span: 0.83 m
Weight with booster: 784.7 kg/924 kg
Weight without booster: 621.4 kg
Max speed: M0.85
Range: approx 130 n miles (240 km)/51 n miles (95 km)
Contractor
Boeing Company, Military Aircraft & Missile Systems Group.
UPDATED

A ship-launched SLAM is fired from the USS Lake Champlain

An RGM-84A is fired from the cruiser USS Leahy which has now been decommissioned (US Navy)

An RGM-84 fired from the `Spruance' class destroyer USS Fletcher. Notice the arrangement of the Mk 141
launcher-containers (US Navy)

A Harpoon is launched from an ASROC launcher

The Spanish `Descubierta' class frigates, such as Cazadora, normally embark only two pairs of Harpoon
launchers. One pair is pictured here (Stefan Terzibaschitsch)

A Sub-Harpoon emerges from the water

A diagram showing the capabilities of Harpoon Block 1 (A and B) compared with Block 1C

A diagram of the AN/SWG-1A(V) Harpoon weapon control system

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От	Олег Радько
К	apple16 (26.11.2002 15:19:39)
Дата	26.11.2002 19:17:51

Cпасибо - видно (-)

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От	Mike
К	Олег Радько (23.11.2002 22:28:26)
Дата	23.11.2002 22:42:01

зреть здесь

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>Добрый день!
>Хотел Вас спросить, нет ли чего в вашем janes по ПЛУР ASROC и IKARA, а также ПКР Sea Skua, AS.34 Kormoran 1/2 и Gabriel...

http://www.fas.org/man/dod-101/sys/missile/row/index.html

а тут американцы

http://www.fas.org/man/dod-101/sys/missile/index.html

С уважением, Mike.

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От	Олег Радько
К	Mike (23.11.2002 22:42:01)
Дата	23.11.2002 22:54:21

В Джейнс гораздо полнее...

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Добрый день!
История разработки и пр..
>>Добрый день!
>>Хотел Вас спросить, нет ли чего в вашем janes по ПЛУР ASROC и IKARA, а также ПКР Sea Skua, AS.34 Kormoran 1/2 и Gabriel...
>
> http://www.fas.org/man/dod-101/sys/missile/row/index.html

>а тут американцы

> http://www.fas.org/man/dod-101/sys/missile/index.html

>С уважением, Mike.
С уважением.

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От	Venik
К	Олег Радько (23.11.2002 22:54:21)
Дата	24.11.2002 00:17:51

Re: В Джейнс

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Мое почтение!

http://212.188.13.195/nvk/forum/files/Venik/vif2_for_oleg_radko.pdf

250Kb

С уважением, Venik

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От	Олег Радько
К	Venik (24.11.2002 00:17:51)
Дата	24.11.2002 00:22:26

спасибо! (-)

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