【翻译】关于A/R/GM-84系列导弹

http://www.designation-systems.net/dusrm/m-84.html
粗暴机翻，只为辟谣鱼叉只有110公里射程。内容不对之处，请见谅

波音（麦道公司）AGM/RGM/UGM-84 鱼叉

The Harpoon is the only dedicated anti-ship missile in service with U.S. armed forces. It has been developed into several advanced versions, including the SLAM (Stand-off Land Attack Missile) derivatives for high-precision attacks on land targets. The Harpoon and SLAM will remain in service with the U.S. Navy for the foreseeable future.

In 1965 the U.S. Navy began studies for a missile in the 45 km (25 nm) range class for use against surfaced submarines. The name Harpoon was assigned to the project (i.e. a harpoon to kill "whales", a naval slang term for submarines). After the sinking of the Isreali destroyer Eilat in 1967 by Soviet-built anti-ship missiles, the U.S. Navy saw the need to develop a dedicated anti-shipping missile, and therefore Harpoon's primary mission became surface ship attack. The development project was formally begun in 1968, and the missile designator ZAGM-84A was allocated in 1970 after the Navy had issued a formal RFP (Request For Proposals). In June 1971, McDonnell Douglas was awarded the prime contract for Harpoon, and the first test missile flew in October 1972. By that time it had already been decided to develop air-launched, ship-launched and submarine-launched Harpoon variants, designated AGM-84A, RGM-84A and UGM-84A, respectively. Because the range requirement was increased to 90 km (50 nm), turbojet propulsion was selected by McDonnell Douglas. Production of the Harpoon began in 1975, and the first version to enter service was the shipborne RGM-84A in 1977, followed by the AGM-84A on P-3 aircraft in 1979. The UGM-84A became operational on attack submarines in 1981. There are also unarmed training versions of the AGM/RGM/UGM-84A, designated ATM-84A, RTM-84A and UTM-84A.


      “鱼叉”是唯一专门为反舰导弹与美国军队服务。它已经发展成为一些先进的版本，包括高精确攻击陆地目标的SLAM（防区外对地攻击导弹）衍生物。鱼叉和SLAM服务与美国海军在可预见的未来将继续留在。

1965年，美国海军开始研究导弹在45公里（25纳米）范围类对浮现潜艇使用。鱼叉被分配到项目的名称 （即杀“鲸鱼”鱼叉俚语，海军潜艇）。后沉没的埃拉特 Isreali驱逐舰于1967年由苏联制造的反舰导弹，美国海军认为有必要开发一个专用的防航运导弹，因此，鱼叉的主要使命成为水面舰艇的攻击。开发项目正式开始于1968年，在1970年和导弹的指示符ZAGM-84A被分配后，海军已正式发布了征求建议书（RFP）。1971年6月，麦道公司被授予合同的主要鱼叉，1972年10月第一次测试导弹飞行。到那个时候已经决定发展航空推出，船舶启动，潜射“鱼叉”的变种，AGM-84A，RGM-84A和 UGM-84A，分别。因为范围的要求提高到90公里（50纳米），麦道公司被选为由涡轮喷气发动机推进。开始于1975年，生产的“鱼叉”和进入服役的第一个版本是舰载RGM-84A于1977年，随后在P-3型飞机于1979年AGM-84A。UGM-84A攻击潜艇于1981年开始运作。也有，ATM-84A，RTM-84A和UTM-84A的的徒手训练的AGM/RGM/UGM-84A版本。

The Harpoon missile is powered by a Teledyne/CAE J402 turbojet in an A/B44G-1 propulsion section, giving it a maximum range of about 185 km (100 nm) for the air-launched version. For surface launches, RGM/UGM-84 variants use a solid-fueled rocket booster in an A/B44G-2 or -3 booster section, which is discarded after burn-out. Maximum range for surface launches is around 140 km (75 nm). After launch, the missile is guided towards the target location as determined by the launching aircraft or ship by a three-axis Attitude Reference Assembly (ATA) in an AN/DSQ-44 guidance section. The ATA is less accurate than a full-fledged inertial system, but good enough for Harpoon's range. For stabilization and control, the AGM-84A has four fixed cruciform wings (3x BSU-42/B, 1x BSU-43/B) and four movable BSU-44/B tailfins. The missile flies at a low cruise altitude, and at a predetermined distance from the expected target position, its AN/DSQ-28 J-band active radar seeker in the nose is activated to acquire and lock on the target. The radar switch-on distance can be set to lower or higher values, the former requiring a more precisely known target location but reducing the risk to be fooled by enemy ECM. An alternative launch mode is called BOL (Bearing-Only Launch). In this mode, the missile is launched in the general direction of the target, and its radar activated from the beginning to scan for the target in a +/- 45° sector in front of the flight path. Once a target has been located and the seeker locked, the xGM-84A missile climbs rapidly to about 1800 m before diving on the target ("pop-up manoeuver"). The 221 kg (488 lb) WDU-18/B penetrating blast-fragmentation warhead (in the WAU-3(V)/B warhead section) is triggered by a time-delayed impact fuze. When no target can be acquired after radar activation, the Harpoon will self-destruct.

The RGM-84A is usually fired from MK 140 (light weight) or MK 141 (shock-hardened) canister launchers, which hold four missiles, but older MK 112 (ASROC) or MK 26 (Standard) launchers can also be used. The RGM-84A has folding wings and fins which flip out immediately after exit from the launcher. For target acquisition and tracking, Harpoon-equipped surface ships use the AN/SWG-1 Harpoon Fire Control System.

     鱼叉“导弹是由一个Teledyne公司/ CAE J402涡轮喷气发动机一个A/B44G-1推进节，给它的最大射程约185公里（100纳米）的空射版本。表面发射，RGM/UGM-84变种，使用固体燃料火箭助推器或-3一个A/B44G-2的助推器部分，这是烧出后丢弃。表面发射最大射程约140公里（75海里）。发射后，导弹是朝着目标位置确定三轴姿态参考大会（ATA）在的AN/DSQ-44指导部分由发射飞机或船舶。ATA是不准确的比一个完整的惯性系统，但不够好鱼叉范围的。AGM-84A的稳定和控制，有四个固定的十字形的翅膀（3 BSU-42 / B，1个BSU-43 / B）和四个可移动BSU-44 / B尾翼。该型导弹在低巡航高度飞行，并在预定的距离预期目标位置，其AN/DSQ-28的J波段主动雷达导引头在鼻子被激活，以获取和锁定目标。雷达开关的距离可以设置为较低或较高值，前者需要更精确地已知的目标位置，但减少的风险被愚弄敌人ECM。另一种发射模式被称为BOL（轴承只能启动）。在这种模式下，导弹的推出在大方向上的目标，并激活其雷达目标的飞行路径前面的+ / - 45°部门从一开始就扫描。一旦目标已经确定，并且x GM-84A导弹的导引头锁定，迅速 ​​攀升至约1800目标上潜水前m（“弹出式机动飞行”）。WDU-18 / B穿透爆炸破片战斗部（WAU-3（V）/ B弹头部分）221公斤（488磅）触发一个时间延迟的影响引信。当没有目标的雷达激活后，可以被收购，鱼叉将自毁。

RGM-84A通常是从MK 140（重量轻）或MK 141（冲击硬化）筒发射，拥有四个导弹，但也可用于老MK 112（阿斯洛克）的MK 26（标准）发射发射。RGM-84A折叠机翼和鳍翻转后立即退出发射。目标捕获和跟踪，水面舰艇配备鱼叉使用AN/SWG-1鱼叉火控系统。



For launch from submarines, the UGM-84A is enclosed in a capsule, which glides to the surface after launch from the torpedo tube. When the capsule breaks the surface, the front and end caps are ejected and the missile fired. The digital MK 117 Fire Control System has full support for Harpoon integrated.

The UGM-84B is a UGM-84A variant for use by the Royal Navy, and flies at a slightly lower cruising altitude than the -84A. The UGM-84B is called GWS-60 by the Royal Navy, and the UTM-84B is the corresponding training version. Interestingly, the designations AGM-84B, RGM-84B, ATM-84B and RTM-84B were also formally allocated, although no air- or ship-launched -84B missiles were ever built.

The next U.S. Navy variant was the Harpoon Block 1B, designated AGM-84C, RGM-84C and UGM-84C. The Block 1B missiles were first delivered to the Navy in June 1982. The xGM-84C flies at the same lower cruise altitude as the UGM-84B, and does no pop-up manoeuver, flying a sea-skimming attack profile instead. The Block 1B training missiles are the ATM-84C, RTM-84C and UTM-84C.


从潜艇发射的UGM-84A的封闭胶囊，从鱼雷发射管发射后的表面下滑。当胶囊打破了表面，正面和端盖弹出并发射导弹。MK 117的数字火控系统具有全力支持集成鱼叉。

UGM-84B是一个由皇家海军使用的UGM-84A的变体，过得比-84A巡航高度稍低。UGM-84B是由皇家海军称为GWS-60，和UTM-84B的是相应的培训版本。有趣的是，名称RGM-84B，AGM-84B，ATM-84B 和RTM-84B的正式分配，虽然没有空中或舰射-84B导弹是有史以来建造。

未来美国海军的变形是的鱼叉座1B，AGM-84C，RGM-84C和UGM-84C的。座1B导弹首次在1982年6月交付给海军。x GM-84C为UGM-84B相同的低巡航高度飞行，并不会弹出的机动飞行，飞行掠海攻击的配置文件而不是。座1B的训练导弹是在 ATM-84C，RTM-84C和UTM-84C的。


In 1985 the Block 1C version of Harpoon was introduced, being designated AGM-84D, RGM-84D and UGM-84D. The Block 1C has increased range (AGM-84D maximum range is quoted to be 220 km (120 nm)) by using JP-10 instead of JP-6 jet fuel. The terminal attack mode of the xGM-84D is selectable (pop-up or sea-skimming), and the missile also has improved ECCM equipment. Ships equipped with the improved AN/SWG-1A Fire Control System can program several way-points into the flight path of the missile before launch. Using this feature, the RGM-84D will fly an indirect path to the target area, thereby concealing the position of the launching ship. As with the earlier versions, there are also ATM-84D, RTM-84D and UTM-84D training missiles. The CATM-84D is a captive-carry training missile. The CATM-84D-1s are converted older ATM-84As, and CATM-84D-2s are improved new-built missiles.

The AGM-84E Harpoon Block 1E SLAM (Stand-off Land Attack Missile) is essentially a new missile. It is a high precision land-attack missile, which combines the airframe, engine and warhead of the anti-ship Harpoon with the WGU-10/B IIR seeker of the AGM-65D Maverick and the data link of the AGM-62 Walleye. Development of SLAM began in 1986 as an interim precision-attack missile pending delivery of the AGM-137 TSSAM (Tri-Service Standoff Attack Missile), and the first all-up AGM-84E rounds were delivered in November 1988. SLAM became operational with the U.S. Navy in 1990, just ready for a few missiles to be used in action in Operation Desert Storm in early 1991. After the TSSAM was cancelled in 1995, the importance of SLAM increased significantly. The AGM-84E flies a complex path to its target using its inertial system, and during the final 60 seconds of the flight it is controlled through the data link (using an AN/AWW-13 pod on the launching aircraft) using imagery from the IIR seeker. The WDU-18/B warhead is in a new WAU-23/B warhead section with an (optionally delayed) impact fuze.

1985年鱼叉 1C座版本，被指定的AGM-84D，RGM-84D和UGM-84D的。座1C增加范围（AGM-84D最大射程220公里（120纳米）报价）使用JP-10，而不是JP-6喷气燃料。终端攻击模式可选（弹出或掠海），x GM-84D导弹也提高了抗干 ​​扰设备。改进AN/SWG-1A的火控系统配备的船舶可以设定几种方法点之前发射的导弹的飞行路径。RGM-84D使用此功能，将飞的间接路径到目标区域，从而隐瞒发射船的位置。与早期版本，也有ATM-84D，RTM-84D和UTM-84D的的训练导弹。CATM-84D是一个俘虏进行训练导弹。CATM-84D-1转换旧的ATM-84As，CATM-84D-2提高了新建导弹。

鱼叉“ AGM-84E 座1E 防区外对地攻击导弹（SLAM）本质上是一种新的导弹。它是一种高精度对地攻击导弹，它结合了WGU-10 / B IIR导引的 AGM-65D的特立独行和数据链路的AGM-62 沃莱反舰“鱼叉”的机体，发动机和弹头。作为一项临时的精确攻击导弹的AGM-137 TSSAM的 （三军防区外攻击导弹）待交付的SLAM的发展 始于1986年，并在1988年11月交付第一台全AGM-84E轮的SLAM开始运作美国海军于1990年，刚准备用在行动“沙漠风暴”行动中，1991年初几枚导弹。后在1995年被取消TSSAM，SLAM的重要性显着提高。AGM-84E飞了复杂的路径目标使用其惯性系统，并在最后60秒的飞行控制，通过使用图像从数据链路（发射飞机上使用一个AN/AWW-13荚） IIR导引头。WDU-18 / B战斗部是在一个新的WAU-23 / B（可选延迟）冲击引信弹头部分。

Non-tactical versions of SLAM include the ATM-84E training missile, CATM-84E captive-carry variant, DATM-84E ground handling trainer, and the NAEM-84E test and evaluation missile with special telemetry equipment. A ship-launched version of SLAM, to be designated RGM-84E Sea-SLAM, was also tested, but production was cancelled.

The next version of the Harpoon anti-ship missile was the Block 1D, designated AGM-84F and RGM-84F. The Block 1D missile was longer and heavier for a significant increase in fuel load and flight duration. Because the increased length prevented the use from submarines, there was no "UGM-84F". The longer duration not only increased the missile's range, but also allowed the integration of a re-attack capability. When the radar seeker could not acquire a target after being switched on, the xGM-84F would fly a cloverleaf-shaped search pattern trying to detect the target until fuel exhaustion. Development of the Block 1D started in 1989, and the first missile flew in September 1991. Although it was planned to convert many Block 1C missiles to Block 1D standard, the program was cancelled in 1993.

The AGM-84G, RGM-84G and UGM-84G Harpoon Block 1G is an upgrade of the xGM-84D Block 1C, the main new feature being the re-attack capability of the xGM-84F Block 1D. In addition, the Block 1G has also further improved ECCM capability. Block 1G missiles will be produced by converting older Block 1C rounds.

The AGM-84H SLAM-ER (Stand-off Land Attack Missile - Expanded Response) is a much improved AGM-84E. Development began in 1994, and the first flight test occurred in March 1997. The first production missiles were delivered to the Navy in April 1998, and IOC (Initial Operational capability) was eventually reached in March 2000. The most prominent new feature of the AGM-84H are the pop-out swept wings (similar to those of the RGM/UGM-109 Tomahawk), which significantly increase the missile's range and manoeuverability. The new AN/DSQ-61 guidance section includes the computers, the inertial system, and the new multi-channel GPS receiver. The data link has a longer range and is more jamming-resistant. Software upgrades in the WCU-24/B control section make it easier for the operator to direct the missile to the selected target, and also introduce such features as target switching immediately before launch and search-while-track mode to search for a better aim-point without breaking lock on an existing one. The IIR seeker is hardened against laser countermeasures and last but not least, the AGM-84H has a much heavier 360 kg (800 lb) WDU-40/B penetrating blast-fragmentation warhead in a WAU-30/B warhead section. Training versions of SLAM-ER are the ATM-84H (with AN/DKT-81 telemetry equipment), CATM-84H and DATM-84H.

斯拉姆非战术的版本，包括ATM-84E训练弹，CATM-84E俘虏进行变异，地勤教练DATM-84E，和NAEM-84E的专用遥测设备的测试和评估导弹。船推出的版本SLAM，被指定RGM-84E 海SLAM，也被测试，但被取消了生产。

下一个版本的“鱼叉”反舰导弹，AGM-84F和RGM-84F座1D 。座1D导弹显著增加载油量和飞行时间较长，较重的。因为长度增加防止潜艇使用，有没有“UGM-84F”。持续时间较长，不仅增加了导弹的射程，但也允许重新攻击能力的整合。当无法获得目标的雷达导引头，在接通电源之后，x GM-84F将试图探测到目标物，直到燃料耗尽飞三叶草形搜索模式。座1D发展开始于1989年，1991年9月第一枚导弹飞。虽然它计划把许多块1C导弹座1D标准，这项计划在1993年取消。

AGM-84G，RGM-84G和UGM-84G的 鱼叉座1G x GM-84D座1C x GM-84F座1D 再攻击能力，主要的新功能的升级。此外，1G座也有进一步提高抗干扰能力。座1G导弹的将被生产，转换旧座1C轮。

AGM-84H“ （SLAM-ER防区外对地攻击导弹-扩大响应）是一个很大的提高，AGM-84E。开发于1994年，并在1997年3月发生的第一次飞行试验。第一条生产导弹，在1998年4月交付海军，并最终于2000年3月达成IOC（初始作战能力）。AGM-84H最突出的新功能是弹出出风靡的翅（类似战斧 RGM/UGM-109的），从而大大提高导弹的射程和操纵性。新AN/DSQ-61指导部包括计算机，惯性系统，新的多通道GPS接收机。数据链路有一个较长的范围，并且更耐干扰。WCU-24 / B控制部分的软件升级，使其更容易为运营商直接到选定的目标导弹，并介绍等功能为目标之前发布和搜索，而双轨模式立即切换到一个更好的目的搜索点而不会破坏现有的锁。IIR导引头对激光对抗硬化，最后但并非最不重要的一点是，AGM-84H有一个更的较重的360千克（800磅）WDU-40 / B穿透爆炸破片战斗部在WAU-30 / B弹头部分。SLAM-ER的训练版本的ATM-84H（遥测设备AN/DKT-81），CATM-84H 和84H DATM。




As early as 1996, McDonnell Douglas proposed the "Harpoon 2000" improvement, later evolving into the Harpoon Block II. Suggested Block II features included a GPS-aided INS, a radar seeker with improved ECCM and some SLAM hardware. The GPS/INS guidance would allow much higher precision in attacks on shore-based targets. The "Harpoon 2000"/Block II proposal was apparently not too well received by the U.S. Navy, and no development order came forward. However, Block II was developed for export as AGM/RGM-84L, q.v.. In February 2008, the designations AGM-84J and RGM-84J were retroactively allocated to Block II conversions based on the AGM-84D.

The AGM-84K is an upgraded variant of the AGM-84H SLAM-ER with internal improvements. Developmental tests of the hardware and software updates of the AGM-84K were conducted in early 2001, followed by operational test and evaluation in the first half of 2002, and Initial Operational Capability in July 2002. Existing AGM-84Hs will be upgraded to AGM-84K standard. Training versions are the ATM-84K and CATM-84K.

The latest upgrade of the AGM-84H/K SLAM-ER is the SLAM-ER ATA (Automatic Target Acquisition). This missile can be launched in the general direction of the target and will automatically select a target by comparing the stored reference image with the IIR seeker image without the need for operator intervention. However, the operator can take over control of the missile at any time in the mission, thereby retaining the capabilities of the basic SLAM-ER. The ATA system was released to the Fleet in 2002, and existing AGM-84H/K missiles will eventually be upgraded.

Although the GPS-equipped Harpoon Block II was not ordered by the U.S. Navy, the missile was offered for export, and eventually ordered by several contries, including Egypt, the United Arab Emirates, Taiwan, and South Korea. These export missiles are based on the RGM-84G, and designated RGM-84L. Korea has also ordered the air-launched AGM-84L variant.

早在1996年，麦道公司提出了“鱼叉”2000“的改进，后来演变成鱼叉“ Block II型。建议第二座设有包括一个GPS辅助导航系统，雷达导引头，改进的抗干扰和一些SLAM硬件。GPS / INS制导会允许攻击岸基目标精度更高。“鱼叉”2000“/第二座建议显然不是太清楚收到由美国海军，并没有开发秩序出面。然而，第二座被开发用于出口为AGM/RGM-84L，QV。在2008年2月，追溯被分配到指定 的AGM-84J和RGM-84J基于AGM-84D Block II型转换。

AGM-84K的升级变种的AGM-84H“ 斯拉姆-ER内部改进。2001年初进行发展测试AGM-84K的硬件和软件的更新，其次是作战测试和评估，在2002年上半年，在2002年7月具备初始作战能力。现有的AGM-84Hs将升级为AGM-84K标准。培训版本的ATM-84K和CATM-84K。

AGM-84H / K SLAM-ER的最新升级的SLAM-ER的 ATA（自动目标捕获）。可以发射这种导弹在目标的大方向，会自动选择一个存储的参考图像与IIR导引头图像，而不需要操作员干预的目标。但是，操作员可以接管控制导弹的使命在任何时间，从而保留了SLAM-ER的基本能力。ATA系统释放的舰队于2002年，现有的AGM-84H / K导弹最终将被升级。

虽然没有下令美国海军配备GPS 鱼叉“ Block II型导弹用于出口，并最终下令由的几个CONTRIES，包括埃及，阿拉伯联合大公国，台湾和韩国。这些出口的导弹是基于RGM-84G，并指定RGM-84L。韩国也下令空中发射的AGM-84L的变体。


In January 2008, the U.S. Navy awarded Boeing an SDD (System Design and Development) contract for the AGM-84M Harpoon Block III. The Block III upgrade includes the major Block II features like the GPS/INS guidance and a new seeker, and adds a two-way datalink. The datalink makes it possible to update the targeting information after launch and actively control the missile at all points of the mission. The Navy plans to acquire Block III upgrade kits for 850 Harpoon missiles, with IOC planned for 2011. The RGM-84M is the ship-launched variant of the Block III missile.

More than 7000 Harpoon anti-ship missiles (including production for foreign countries) and 1000 SLAM variants have been built so far. Production of the anti-ship missiles continues for non-US customers, while productuon for the U.S. Navy will continue with the AGM-84K SLAM-ER ATA. Current U.S. platforms for the AGM-84 anti-ship Harpoon are the Navy's F/A-18, P-3C and S-3B and also a few B-52Hs of the USAF. The AGM-84E/H/K SLAM is mainly employed by the F/A-18, but has been used by the P-3C, too.

Specifications

Note: Data given by several sources show slight variations. Figures given below may therefore be inaccurate!

Data for AGM-84D/E/F/H/K, RGM/UGM-84D (incl. booster):

        AGM-84D        RGM/UGM-84D        AGM-84E        AGM-84F        AGM-84H/K
Length        3.85 m (12 ft 7.5 in)        4.63 m (15 ft 2.2 in)        4.50 m (14 ft 9 in)        4.44 m (14 ft 6.9 in)        4.37 m (14 ft 4 in)
Wingspan        91.4 cm (36 in)        2.43 m (96 in)
Diameter        34.3 cm (13.5 in)
Weight        540 kg (1200 lb)        690 kg (1520 lb)        627 kg (1385 lb)        635 kg (1400 lb)        725 kg (1600 lb)
Speed        Mach 0.85
Range        220 km (120 nm)        140 km (75 nm)        93 km (50 nm)        315 km (170 nm)        280 km (150 nm)
Propulsion        Sustainer: Teledyne/CAE J402-CA-400 turbojet; 3.0 kN (680 lb)
Booster (RGM/UGM-84 only): A/B44G-2 or -3 solid-fueled rocket; 53 kN (12000 lb) for 2.9 sec
Warhead        221 kg (488 lb) WDU-18/B penetrating blast-fragmentation        360 kg (800 lb) WDU-40/B penetrating BF
Main Sources

[1] Norman Friedman: "US Naval Weapons", Conway Maritime Press, 1983
[2] Norman Friedman: "World Naval Weapons Systems, 1997/98", Naval Institute Press, 1997
[3] Christopher Chant: "World Encyclopaedia of Modern Air Weapons", Patrick Stephens Ltd., 1988
[4] Hajime Ozu: "Missile 2000 - Reference Guide to World Missile Systems", Shinkigensha, 2000
[5] Bernard Blake (ed.): "Jane's Weapon Systems 1987-88", Jane's, 1988


Back to Current Designations Of U.S. Unmanned Military Aerospace Vehicles
Back to Directory of U.S. Military Rockets and Missiles

2008年1月，美国海军授予波音公司的AGM-84M“ 鱼叉“Block III型系统设计与开发（SDD）合同。Block III的升级包括主要的Block II型功能，如GPS / INS制导和新型导引头，并增加了一个双向数据链。数据链，使得它可以在发射后的目标信息更新，并积极控制导弹的所有点的使命。海军计划收购Block III的升级包为850 枚“鱼叉”导弹，计划于2011年与国际奥委会。RGM-84M 的Block III型导弹是舰射的变种。

到目前为止，已建成超过7000 枚“鱼叉”（Harpoon）反舰导弹（包括外国生产）和1000 SLAM变种。非美国客户继续生产的反舰导弹，AGM-84K SLAM-ER ATA 而为美国海军productuon将继续。AGM-84反舰“鱼叉”是美国目前的平台海军的F/A-18，P-3C和S-3B，也有少数的美国空军B-52Hs。AGM-84E/H/K SLAM主要采用的F/A-18，但一直使用的P-3C也。

产品规格

注：由几个来源的数据显示轻微的变化。下面给出的数字，因此可能是不准确的！

，RGM/UGM-84D AGM-84D/E/F/H/K（含增压）的数据：

        AGM-84D        RGM/UGM-84D        AGM-84E        AGM-84F        AGM-84H / K
长度        3.85米（12英尺7.5英寸）        4.63米（15英尺2.2英寸）        4.50米（14呎9）        4.44米（14英尺6.9英寸）        4.37米（14英尺4英寸）
翼展        91.4厘米（36）        2.43米（96）
直径        34.3厘米（13.5）
重量        540公斤（1200磅）        690公斤（1520磅）        627千克（1385磅）        635公斤（1400磅）        725公斤（1600磅）
速度        0.85马赫
范围        220公里（120纳米）        140公里（75海里）        93公里（50纳米）        315公里（170海里）        280公里（150海里）
动力        自持：Teledyne公司/ CAE J402-CA-400涡喷发动机，3.0千牛（680磅）
助推器（仅RGM/UGM-84）：在A/B44G-2或-3固体燃料火箭; 53千牛（12000磅）的2.9秒
弹头        （488磅）221千克WDU-18 / B穿透爆炸破片        360公斤（800磅）WDU-40 / B BF穿透
主要来源

[1]诺曼·弗里德曼：“美国海军武器”，康威海事出版社，1983
[2]诺曼·弗里德曼：“世界海军武器系统，1997/98”，海军学院出版社，1997年
[3]克里斯托弗·咏：“世界现代百科全书航空武器“，帕特里克·斯蒂芬斯有限公司，1988
[4]小津安二郎肇：“导弹2000年-世界导弹系统的参考指南”，Shinkigensha，2000
[5]伯纳德·布莱克（主编）：“简氏武器系统1987-88赛季”简氏1988年


另附表一张。如下
链接在此：http://www.areamilitar.net/DIRECTORIO/MIS.aspx?nm=267

Série        Modelo        Alcance        ano
Block I
RGM-84A        80km        1977
UGM-84A        80km        1981
AGM-84A        90km        1979
UGM-84B (Royal Navy GWS-60)        90km        1981
Block 1b
RGM-84C        124km        1982
AGM-84C        220km        1982
UGM-84C        124km        1982
Block 1c
RGM-84D        124km        1985
UGM-84D        124km        1985
AGM-84D        220km        1985
        AGM-84E SLAM        93km        1988
Block 1d
(cancelado)
RGM-84F        315km        1991
AGM-84F        315km        1991
Block 1G
(Block 1c modificado)
AGM-84G        220km        1995
RGM-84G        124km        1995
UGM-84G        124km        1995
        AGM-84H SLAM-ER        280km        2002
        AGM-84K SLAM-ER modificado        280km        2002
Block II
AGM-84L        280/50km        2002
RGM-84L        280/50km        2002
UGM-84L        280/50km        2002
Block III
AGM-84M        220km        2011
RGM-84M        124km        2011
UGM-84M         



http://www.designation-systems.net/dusrm/m-84.html
粗暴机翻，只为辟谣鱼叉只有110公里射程。内容不对之处，请见谅
波音（麦道公司）AGM/RGM/UGM-84 鱼叉


The Harpoon is the only dedicated anti-ship missile in service with U.S. armed forces. It has been developed into several advanced versions, including the SLAM (Stand-off Land Attack Missile) derivatives for high-precision attacks on land targets. The Harpoon and SLAM will remain in service with the U.S. Navy for the foreseeable future.

In 1965 the U.S. Navy began studies for a missile in the 45 km (25 nm) range class for use against surfaced submarines. The name Harpoon was assigned to the project (i.e. a harpoon to kill "whales", a naval slang term for submarines). After the sinking of the Isreali destroyer Eilat in 1967 by Soviet-built anti-ship missiles, the U.S. Navy saw the need to develop a dedicated anti-shipping missile, and therefore Harpoon's primary mission became surface ship attack. The development project was formally begun in 1968, and the missile designator ZAGM-84A was allocated in 1970 after the Navy had issued a formal RFP (Request For Proposals). In June 1971, McDonnell Douglas was awarded the prime contract for Harpoon, and the first test missile flew in October 1972. By that time it had already been decided to develop air-launched, ship-launched and submarine-launched Harpoon variants, designated AGM-84A, RGM-84A and UGM-84A, respectively. Because the range requirement was increased to 90 km (50 nm), turbojet propulsion was selected by McDonnell Douglas. Production of the Harpoon began in 1975, and the first version to enter service was the shipborne RGM-84A in 1977, followed by the AGM-84A on P-3 aircraft in 1979. The UGM-84A became operational on attack submarines in 1981. There are also unarmed training versions of the AGM/RGM/UGM-84A, designated ATM-84A, RTM-84A and UTM-84A.


      “鱼叉”是唯一专门为反舰导弹与美国军队服务。它已经发展成为一些先进的版本，包括高精确攻击陆地目标的SLAM（防区外对地攻击导弹）衍生物。鱼叉和SLAM服务与美国海军在可预见的未来将继续留在。

1965年，美国海军开始研究导弹在45公里（25纳米）范围类对浮现潜艇使用。鱼叉被分配到项目的名称 （即杀“鲸鱼”鱼叉俚语，海军潜艇）。后沉没的埃拉特 Isreali驱逐舰于1967年由苏联制造的反舰导弹，美国海军认为有必要开发一个专用的防航运导弹，因此，鱼叉的主要使命成为水面舰艇的攻击。开发项目正式开始于1968年，在1970年和导弹的指示符ZAGM-84A被分配后，海军已正式发布了征求建议书（RFP）。1971年6月，麦道公司被授予合同的主要鱼叉，1972年10月第一次测试导弹飞行。到那个时候已经决定发展航空推出，船舶启动，潜射“鱼叉”的变种，AGM-84A，RGM-84A和 UGM-84A，分别。因为范围的要求提高到90公里（50纳米），麦道公司被选为由涡轮喷气发动机推进。开始于1975年，生产的“鱼叉”和进入服役的第一个版本是舰载RGM-84A于1977年，随后在P-3型飞机于1979年AGM-84A。UGM-84A攻击潜艇于1981年开始运作。也有，ATM-84A，RTM-84A和UTM-84A的的徒手训练的AGM/RGM/UGM-84A版本。

The Harpoon missile is powered by a Teledyne/CAE J402 turbojet in an A/B44G-1 propulsion section, giving it a maximum range of about 185 km (100 nm) for the air-launched version. For surface launches, RGM/UGM-84 variants use a solid-fueled rocket booster in an A/B44G-2 or -3 booster section, which is discarded after burn-out. Maximum range for surface launches is around 140 km (75 nm). After launch, the missile is guided towards the target location as determined by the launching aircraft or ship by a three-axis Attitude Reference Assembly (ATA) in an AN/DSQ-44 guidance section. The ATA is less accurate than a full-fledged inertial system, but good enough for Harpoon's range. For stabilization and control, the AGM-84A has four fixed cruciform wings (3x BSU-42/B, 1x BSU-43/B) and four movable BSU-44/B tailfins. The missile flies at a low cruise altitude, and at a predetermined distance from the expected target position, its AN/DSQ-28 J-band active radar seeker in the nose is activated to acquire and lock on the target. The radar switch-on distance can be set to lower or higher values, the former requiring a more precisely known target location but reducing the risk to be fooled by enemy ECM. An alternative launch mode is called BOL (Bearing-Only Launch). In this mode, the missile is launched in the general direction of the target, and its radar activated from the beginning to scan for the target in a +/- 45° sector in front of the flight path. Once a target has been located and the seeker locked, the xGM-84A missile climbs rapidly to about 1800 m before diving on the target ("pop-up manoeuver"). The 221 kg (488 lb) WDU-18/B penetrating blast-fragmentation warhead (in the WAU-3(V)/B warhead section) is triggered by a time-delayed impact fuze. When no target can be acquired after radar activation, the Harpoon will self-destruct.

The RGM-84A is usually fired from MK 140 (light weight) or MK 141 (shock-hardened) canister launchers, which hold four missiles, but older MK 112 (ASROC) or MK 26 (Standard) launchers can also be used. The RGM-84A has folding wings and fins which flip out immediately after exit from the launcher. For target acquisition and tracking, Harpoon-equipped surface ships use the AN/SWG-1 Harpoon Fire Control System.

     鱼叉“导弹是由一个Teledyne公司/ CAE J402涡轮喷气发动机一个A/B44G-1推进节，给它的最大射程约185公里（100纳米）的空射版本。表面发射，RGM/UGM-84变种，使用固体燃料火箭助推器或-3一个A/B44G-2的助推器部分，这是烧出后丢弃。表面发射最大射程约140公里（75海里）。发射后，导弹是朝着目标位置确定三轴姿态参考大会（ATA）在的AN/DSQ-44指导部分由发射飞机或船舶。ATA是不准确的比一个完整的惯性系统，但不够好鱼叉范围的。AGM-84A的稳定和控制，有四个固定的十字形的翅膀（3 BSU-42 / B，1个BSU-43 / B）和四个可移动BSU-44 / B尾翼。该型导弹在低巡航高度飞行，并在预定的距离预期目标位置，其AN/DSQ-28的J波段主动雷达导引头在鼻子被激活，以获取和锁定目标。雷达开关的距离可以设置为较低或较高值，前者需要更精确地已知的目标位置，但减少的风险被愚弄敌人ECM。另一种发射模式被称为BOL（轴承只能启动）。在这种模式下，导弹的推出在大方向上的目标，并激活其雷达目标的飞行路径前面的+ / - 45°部门从一开始就扫描。一旦目标已经确定，并且x GM-84A导弹的导引头锁定，迅速 ​​攀升至约1800目标上潜水前m（“弹出式机动飞行”）。WDU-18 / B穿透爆炸破片战斗部（WAU-3（V）/ B弹头部分）221公斤（488磅）触发一个时间延迟的影响引信。当没有目标的雷达激活后，可以被收购，鱼叉将自毁。

RGM-84A通常是从MK 140（重量轻）或MK 141（冲击硬化）筒发射，拥有四个导弹，但也可用于老MK 112（阿斯洛克）的MK 26（标准）发射发射。RGM-84A折叠机翼和鳍翻转后立即退出发射。目标捕获和跟踪，水面舰艇配备鱼叉使用AN/SWG-1鱼叉火控系统。



For launch from submarines, the UGM-84A is enclosed in a capsule, which glides to the surface after launch from the torpedo tube. When the capsule breaks the surface, the front and end caps are ejected and the missile fired. The digital MK 117 Fire Control System has full support for Harpoon integrated.

The UGM-84B is a UGM-84A variant for use by the Royal Navy, and flies at a slightly lower cruising altitude than the -84A. The UGM-84B is called GWS-60 by the Royal Navy, and the UTM-84B is the corresponding training version. Interestingly, the designations AGM-84B, RGM-84B, ATM-84B and RTM-84B were also formally allocated, although no air- or ship-launched -84B missiles were ever built.

The next U.S. Navy variant was the Harpoon Block 1B, designated AGM-84C, RGM-84C and UGM-84C. The Block 1B missiles were first delivered to the Navy in June 1982. The xGM-84C flies at the same lower cruise altitude as the UGM-84B, and does no pop-up manoeuver, flying a sea-skimming attack profile instead. The Block 1B training missiles are the ATM-84C, RTM-84C and UTM-84C.


从潜艇发射的UGM-84A的封闭胶囊，从鱼雷发射管发射后的表面下滑。当胶囊打破了表面，正面和端盖弹出并发射导弹。MK 117的数字火控系统具有全力支持集成鱼叉。

UGM-84B是一个由皇家海军使用的UGM-84A的变体，过得比-84A巡航高度稍低。UGM-84B是由皇家海军称为GWS-60，和UTM-84B的是相应的培训版本。有趣的是，名称RGM-84B，AGM-84B，ATM-84B 和RTM-84B的正式分配，虽然没有空中或舰射-84B导弹是有史以来建造。

未来美国海军的变形是的鱼叉座1B，AGM-84C，RGM-84C和UGM-84C的。座1B导弹首次在1982年6月交付给海军。x GM-84C为UGM-84B相同的低巡航高度飞行，并不会弹出的机动飞行，飞行掠海攻击的配置文件而不是。座1B的训练导弹是在 ATM-84C，RTM-84C和UTM-84C的。


In 1985 the Block 1C version of Harpoon was introduced, being designated AGM-84D, RGM-84D and UGM-84D. The Block 1C has increased range (AGM-84D maximum range is quoted to be 220 km (120 nm)) by using JP-10 instead of JP-6 jet fuel. The terminal attack mode of the xGM-84D is selectable (pop-up or sea-skimming), and the missile also has improved ECCM equipment. Ships equipped with the improved AN/SWG-1A Fire Control System can program several way-points into the flight path of the missile before launch. Using this feature, the RGM-84D will fly an indirect path to the target area, thereby concealing the position of the launching ship. As with the earlier versions, there are also ATM-84D, RTM-84D and UTM-84D training missiles. The CATM-84D is a captive-carry training missile. The CATM-84D-1s are converted older ATM-84As, and CATM-84D-2s are improved new-built missiles.

The AGM-84E Harpoon Block 1E SLAM (Stand-off Land Attack Missile) is essentially a new missile. It is a high precision land-attack missile, which combines the airframe, engine and warhead of the anti-ship Harpoon with the WGU-10/B IIR seeker of the AGM-65D Maverick and the data link of the AGM-62 Walleye. Development of SLAM began in 1986 as an interim precision-attack missile pending delivery of the AGM-137 TSSAM (Tri-Service Standoff Attack Missile), and the first all-up AGM-84E rounds were delivered in November 1988. SLAM became operational with the U.S. Navy in 1990, just ready for a few missiles to be used in action in Operation Desert Storm in early 1991. After the TSSAM was cancelled in 1995, the importance of SLAM increased significantly. The AGM-84E flies a complex path to its target using its inertial system, and during the final 60 seconds of the flight it is controlled through the data link (using an AN/AWW-13 pod on the launching aircraft) using imagery from the IIR seeker. The WDU-18/B warhead is in a new WAU-23/B warhead section with an (optionally delayed) impact fuze.

1985年鱼叉 1C座版本，被指定的AGM-84D，RGM-84D和UGM-84D的。座1C增加范围（AGM-84D最大射程220公里（120纳米）报价）使用JP-10，而不是JP-6喷气燃料。终端攻击模式可选（弹出或掠海），x GM-84D导弹也提高了抗干 ​​扰设备。改进AN/SWG-1A的火控系统配备的船舶可以设定几种方法点之前发射的导弹的飞行路径。RGM-84D使用此功能，将飞的间接路径到目标区域，从而隐瞒发射船的位置。与早期版本，也有ATM-84D，RTM-84D和UTM-84D的的训练导弹。CATM-84D是一个俘虏进行训练导弹。CATM-84D-1转换旧的ATM-84As，CATM-84D-2提高了新建导弹。

鱼叉“ AGM-84E 座1E 防区外对地攻击导弹（SLAM）本质上是一种新的导弹。它是一种高精度对地攻击导弹，它结合了WGU-10 / B IIR导引的 AGM-65D的特立独行和数据链路的AGM-62 沃莱反舰“鱼叉”的机体，发动机和弹头。作为一项临时的精确攻击导弹的AGM-137 TSSAM的 （三军防区外攻击导弹）待交付的SLAM的发展 始于1986年，并在1988年11月交付第一台全AGM-84E轮的SLAM开始运作美国海军于1990年，刚准备用在行动“沙漠风暴”行动中，1991年初几枚导弹。后在1995年被取消TSSAM，SLAM的重要性显着提高。AGM-84E飞了复杂的路径目标使用其惯性系统，并在最后60秒的飞行控制，通过使用图像从数据链路（发射飞机上使用一个AN/AWW-13荚） IIR导引头。WDU-18 / B战斗部是在一个新的WAU-23 / B（可选延迟）冲击引信弹头部分。

Non-tactical versions of SLAM include the ATM-84E training missile, CATM-84E captive-carry variant, DATM-84E ground handling trainer, and the NAEM-84E test and evaluation missile with special telemetry equipment. A ship-launched version of SLAM, to be designated RGM-84E Sea-SLAM, was also tested, but production was cancelled.

The next version of the Harpoon anti-ship missile was the Block 1D, designated AGM-84F and RGM-84F. The Block 1D missile was longer and heavier for a significant increase in fuel load and flight duration. Because the increased length prevented the use from submarines, there was no "UGM-84F". The longer duration not only increased the missile's range, but also allowed the integration of a re-attack capability. When the radar seeker could not acquire a target after being switched on, the xGM-84F would fly a cloverleaf-shaped search pattern trying to detect the target until fuel exhaustion. Development of the Block 1D started in 1989, and the first missile flew in September 1991. Although it was planned to convert many Block 1C missiles to Block 1D standard, the program was cancelled in 1993.

The AGM-84G, RGM-84G and UGM-84G Harpoon Block 1G is an upgrade of the xGM-84D Block 1C, the main new feature being the re-attack capability of the xGM-84F Block 1D. In addition, the Block 1G has also further improved ECCM capability. Block 1G missiles will be produced by converting older Block 1C rounds.

The AGM-84H SLAM-ER (Stand-off Land Attack Missile - Expanded Response) is a much improved AGM-84E. Development began in 1994, and the first flight test occurred in March 1997. The first production missiles were delivered to the Navy in April 1998, and IOC (Initial Operational capability) was eventually reached in March 2000. The most prominent new feature of the AGM-84H are the pop-out swept wings (similar to those of the RGM/UGM-109 Tomahawk), which significantly increase the missile's range and manoeuverability. The new AN/DSQ-61 guidance section includes the computers, the inertial system, and the new multi-channel GPS receiver. The data link has a longer range and is more jamming-resistant. Software upgrades in the WCU-24/B control section make it easier for the operator to direct the missile to the selected target, and also introduce such features as target switching immediately before launch and search-while-track mode to search for a better aim-point without breaking lock on an existing one. The IIR seeker is hardened against laser countermeasures and last but not least, the AGM-84H has a much heavier 360 kg (800 lb) WDU-40/B penetrating blast-fragmentation warhead in a WAU-30/B warhead section. Training versions of SLAM-ER are the ATM-84H (with AN/DKT-81 telemetry equipment), CATM-84H and DATM-84H.

斯拉姆非战术的版本，包括ATM-84E训练弹，CATM-84E俘虏进行变异，地勤教练DATM-84E，和NAEM-84E的专用遥测设备的测试和评估导弹。船推出的版本SLAM，被指定RGM-84E 海SLAM，也被测试，但被取消了生产。

下一个版本的“鱼叉”反舰导弹，AGM-84F和RGM-84F座1D 。座1D导弹显著增加载油量和飞行时间较长，较重的。因为长度增加防止潜艇使用，有没有“UGM-84F”。持续时间较长，不仅增加了导弹的射程，但也允许重新攻击能力的整合。当无法获得目标的雷达导引头，在接通电源之后，x GM-84F将试图探测到目标物，直到燃料耗尽飞三叶草形搜索模式。座1D发展开始于1989年，1991年9月第一枚导弹飞。虽然它计划把许多块1C导弹座1D标准，这项计划在1993年取消。

AGM-84G，RGM-84G和UGM-84G的 鱼叉座1G x GM-84D座1C x GM-84F座1D 再攻击能力，主要的新功能的升级。此外，1G座也有进一步提高抗干扰能力。座1G导弹的将被生产，转换旧座1C轮。

AGM-84H“ （SLAM-ER防区外对地攻击导弹-扩大响应）是一个很大的提高，AGM-84E。开发于1994年，并在1997年3月发生的第一次飞行试验。第一条生产导弹，在1998年4月交付海军，并最终于2000年3月达成IOC（初始作战能力）。AGM-84H最突出的新功能是弹出出风靡的翅（类似战斧 RGM/UGM-109的），从而大大提高导弹的射程和操纵性。新AN/DSQ-61指导部包括计算机，惯性系统，新的多通道GPS接收机。数据链路有一个较长的范围，并且更耐干扰。WCU-24 / B控制部分的软件升级，使其更容易为运营商直接到选定的目标导弹，并介绍等功能为目标之前发布和搜索，而双轨模式立即切换到一个更好的目的搜索点而不会破坏现有的锁。IIR导引头对激光对抗硬化，最后但并非最不重要的一点是，AGM-84H有一个更的较重的360千克（800磅）WDU-40 / B穿透爆炸破片战斗部在WAU-30 / B弹头部分。SLAM-ER的训练版本的ATM-84H（遥测设备AN/DKT-81），CATM-84H 和84H DATM。




As early as 1996, McDonnell Douglas proposed the "Harpoon 2000" improvement, later evolving into the Harpoon Block II. Suggested Block II features included a GPS-aided INS, a radar seeker with improved ECCM and some SLAM hardware. The GPS/INS guidance would allow much higher precision in attacks on shore-based targets. The "Harpoon 2000"/Block II proposal was apparently not too well received by the U.S. Navy, and no development order came forward. However, Block II was developed for export as AGM/RGM-84L, q.v.. In February 2008, the designations AGM-84J and RGM-84J were retroactively allocated to Block II conversions based on the AGM-84D.

The AGM-84K is an upgraded variant of the AGM-84H SLAM-ER with internal improvements. Developmental tests of the hardware and software updates of the AGM-84K were conducted in early 2001, followed by operational test and evaluation in the first half of 2002, and Initial Operational Capability in July 2002. Existing AGM-84Hs will be upgraded to AGM-84K standard. Training versions are the ATM-84K and CATM-84K.

The latest upgrade of the AGM-84H/K SLAM-ER is the SLAM-ER ATA (Automatic Target Acquisition). This missile can be launched in the general direction of the target and will automatically select a target by comparing the stored reference image with the IIR seeker image without the need for operator intervention. However, the operator can take over control of the missile at any time in the mission, thereby retaining the capabilities of the basic SLAM-ER. The ATA system was released to the Fleet in 2002, and existing AGM-84H/K missiles will eventually be upgraded.

Although the GPS-equipped Harpoon Block II was not ordered by the U.S. Navy, the missile was offered for export, and eventually ordered by several contries, including Egypt, the United Arab Emirates, Taiwan, and South Korea. These export missiles are based on the RGM-84G, and designated RGM-84L. Korea has also ordered the air-launched AGM-84L variant.

早在1996年，麦道公司提出了“鱼叉”2000“的改进，后来演变成鱼叉“ Block II型。建议第二座设有包括一个GPS辅助导航系统，雷达导引头，改进的抗干扰和一些SLAM硬件。GPS / INS制导会允许攻击岸基目标精度更高。“鱼叉”2000“/第二座建议显然不是太清楚收到由美国海军，并没有开发秩序出面。然而，第二座被开发用于出口为AGM/RGM-84L，QV。在2008年2月，追溯被分配到指定 的AGM-84J和RGM-84J基于AGM-84D Block II型转换。

AGM-84K的升级变种的AGM-84H“ 斯拉姆-ER内部改进。2001年初进行发展测试AGM-84K的硬件和软件的更新，其次是作战测试和评估，在2002年上半年，在2002年7月具备初始作战能力。现有的AGM-84Hs将升级为AGM-84K标准。培训版本的ATM-84K和CATM-84K。

AGM-84H / K SLAM-ER的最新升级的SLAM-ER的 ATA（自动目标捕获）。可以发射这种导弹在目标的大方向，会自动选择一个存储的参考图像与IIR导引头图像，而不需要操作员干预的目标。但是，操作员可以接管控制导弹的使命在任何时间，从而保留了SLAM-ER的基本能力。ATA系统释放的舰队于2002年，现有的AGM-84H / K导弹最终将被升级。

虽然没有下令美国海军配备GPS 鱼叉“ Block II型导弹用于出口，并最终下令由的几个CONTRIES，包括埃及，阿拉伯联合大公国，台湾和韩国。这些出口的导弹是基于RGM-84G，并指定RGM-84L。韩国也下令空中发射的AGM-84L的变体。


In January 2008, the U.S. Navy awarded Boeing an SDD (System Design and Development) contract for the AGM-84M Harpoon Block III. The Block III upgrade includes the major Block II features like the GPS/INS guidance and a new seeker, and adds a two-way datalink. The datalink makes it possible to update the targeting information after launch and actively control the missile at all points of the mission. The Navy plans to acquire Block III upgrade kits for 850 Harpoon missiles, with IOC planned for 2011. The RGM-84M is the ship-launched variant of the Block III missile.

More than 7000 Harpoon anti-ship missiles (including production for foreign countries) and 1000 SLAM variants have been built so far. Production of the anti-ship missiles continues for non-US customers, while productuon for the U.S. Navy will continue with the AGM-84K SLAM-ER ATA. Current U.S. platforms for the AGM-84 anti-ship Harpoon are the Navy's F/A-18, P-3C and S-3B and also a few B-52Hs of the USAF. The AGM-84E/H/K SLAM is mainly employed by the F/A-18, but has been used by the P-3C, too.

Specifications

Note: Data given by several sources show slight variations. Figures given below may therefore be inaccurate!

Data for AGM-84D/E/F/H/K, RGM/UGM-84D (incl. booster):

        AGM-84D        RGM/UGM-84D        AGM-84E        AGM-84F        AGM-84H/K
Length        3.85 m (12 ft 7.5 in)        4.63 m (15 ft 2.2 in)        4.50 m (14 ft 9 in)        4.44 m (14 ft 6.9 in)        4.37 m (14 ft 4 in)
Wingspan        91.4 cm (36 in)        2.43 m (96 in)
Diameter        34.3 cm (13.5 in)
Weight        540 kg (1200 lb)        690 kg (1520 lb)        627 kg (1385 lb)        635 kg (1400 lb)        725 kg (1600 lb)
Speed        Mach 0.85
Range        220 km (120 nm)        140 km (75 nm)        93 km (50 nm)        315 km (170 nm)        280 km (150 nm)
Propulsion        Sustainer: Teledyne/CAE J402-CA-400 turbojet; 3.0 kN (680 lb)
Booster (RGM/UGM-84 only): A/B44G-2 or -3 solid-fueled rocket; 53 kN (12000 lb) for 2.9 sec
Warhead        221 kg (488 lb) WDU-18/B penetrating blast-fragmentation        360 kg (800 lb) WDU-40/B penetrating BF
Main Sources

[1] Norman Friedman: "US Naval Weapons", Conway Maritime Press, 1983
[2] Norman Friedman: "World Naval Weapons Systems, 1997/98", Naval Institute Press, 1997
[3] Christopher Chant: "World Encyclopaedia of Modern Air Weapons", Patrick Stephens Ltd., 1988
[4] Hajime Ozu: "Missile 2000 - Reference Guide to World Missile Systems", Shinkigensha, 2000
[5] Bernard Blake (ed.): "Jane's Weapon Systems 1987-88", Jane's, 1988


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2008年1月，美国海军授予波音公司的AGM-84M“ 鱼叉“Block III型系统设计与开发（SDD）合同。Block III的升级包括主要的Block II型功能，如GPS / INS制导和新型导引头，并增加了一个双向数据链。数据链，使得它可以在发射后的目标信息更新，并积极控制导弹的所有点的使命。海军计划收购Block III的升级包为850 枚“鱼叉”导弹，计划于2011年与国际奥委会。RGM-84M 的Block III型导弹是舰射的变种。

到目前为止，已建成超过7000 枚“鱼叉”（Harpoon）反舰导弹（包括外国生产）和1000 SLAM变种。非美国客户继续生产的反舰导弹，AGM-84K SLAM-ER ATA 而为美国海军productuon将继续。AGM-84反舰“鱼叉”是美国目前的平台海军的F/A-18，P-3C和S-3B，也有少数的美国空军B-52Hs。AGM-84E/H/K SLAM主要采用的F/A-18，但一直使用的P-3C也。

产品规格

注：由几个来源的数据显示轻微的变化。下面给出的数字，因此可能是不准确的！

，RGM/UGM-84D AGM-84D/E/F/H/K（含增压）的数据：

        AGM-84D        RGM/UGM-84D        AGM-84E        AGM-84F        AGM-84H / K
长度        3.85米（12英尺7.5英寸）        4.63米（15英尺2.2英寸）        4.50米（14呎9）        4.44米（14英尺6.9英寸）        4.37米（14英尺4英寸）
翼展        91.4厘米（36）        2.43米（96）
直径        34.3厘米（13.5）
重量        540公斤（1200磅）        690公斤（1520磅）        627千克（1385磅）        635公斤（1400磅）        725公斤（1600磅）
速度        0.85马赫
范围        220公里（120纳米）        140公里（75海里）        93公里（50纳米）        315公里（170海里）        280公里（150海里）
动力        自持：Teledyne公司/ CAE J402-CA-400涡喷发动机，3.0千牛（680磅）
助推器（仅RGM/UGM-84）：在A/B44G-2或-3固体燃料火箭; 53千牛（12000磅）的2.9秒
弹头        （488磅）221千克WDU-18 / B穿透爆炸破片        360公斤（800磅）WDU-40 / B BF穿透
主要来源

[1]诺曼·弗里德曼：“美国海军武器”，康威海事出版社，1983
[2]诺曼·弗里德曼：“世界海军武器系统，1997/98”，海军学院出版社，1997年
[3]克里斯托弗·咏：“世界现代百科全书航空武器“，帕特里克·斯蒂芬斯有限公司，1988
[4]小津安二郎肇：“导弹2000年-世界导弹系统的参考指南”，Shinkigensha，2000
[5]伯纳德·布莱克（主编）：“简氏武器系统1987-88赛季”简氏1988年


另附表一张。如下
链接在此：http://www.areamilitar.net/DIRECTORIO/MIS.aspx?nm=267

Série        Modelo        Alcance        ano
Block I
RGM-84A        80km        1977
UGM-84A        80km        1981
AGM-84A        90km        1979
UGM-84B (Royal Navy GWS-60)        90km        1981
Block 1b
RGM-84C        124km        1982
AGM-84C        220km        1982
UGM-84C        124km        1982
Block 1c
RGM-84D        124km        1985
UGM-84D        124km        1985
AGM-84D        220km        1985
        AGM-84E SLAM        93km        1988
Block 1d
(cancelado)
RGM-84F        315km        1991
AGM-84F        315km        1991
Block 1G
(Block 1c modificado)
AGM-84G        220km        1995
RGM-84G        124km        1995
UGM-84G        124km        1995
        AGM-84H SLAM-ER        280km        2002
        AGM-84K SLAM-ER modificado        280km        2002
Block II
AGM-84L        280/50km        2002
RGM-84L        280/50km        2002
UGM-84L        280/50km        2002
Block III
AGM-84M        220km        2011
RGM-84M        124km        2011
UGM-84M