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The EA-6B Prowler is a carrier based eletronic warfare aircraft developed by Grumman. The primary mission is to protect fleet surface units and other aircraft by jamming hostile radars and communications. In 1995 the EF-111 Raven retired, then left the EA-6B the only radar jammer in DoD. Five new squadrons were stood up, and four of them are dedicated to supporting USAF Aerospace Expeditionary Force wings. The EA-6B is the transition from the EA-6A aircraft. The contract is signed in 1966, first flight in Jan 1971, total production 170 which all deployed before 1991. Marine Tactical Electronic Warfare Squadron 2 (VMAQ-2) continued to provide detachments to Carrier Air Wing Five on board the USS Midway. In 1980 VMAQ-2 completed its assignment aboard the Midway and began shore-based rotations with the 1st Marine Aircraft Wing in Iwakuni, Japan. Detachments were subsequently sent back to sea duty aboard the USS Saratoga and USS America. Marine Prowlers supported from the carrier Navy and Air Force strikes against Libya (1986) during Operation Eldorado Canyon.
The EA-6 is derived from the two-seater A-6 Intruder attack aircraft. The basic airframe was stretched and strengthened to accommodate a four-seat cockpit. Another distinguishing feature is the pod-shaped fairing at the top of the vertical fin. The heart of the EA-6B is the AN/ALQ-99 Tactical Jamming System. And it can carry up to five pods (one belly mounted and two on each wing). Each pod is integrally powered and houses two jamming transmitters that cover one of seven frequency bands. The air fan drives the dynamo to provide power. The EA-6B can carry any mix of pods, fuel tanks and/or AGM-88 HARM anti-radiation missiles depending on mission requirements. The EA-6B's tail fin pod houses sensitive surveillance receivers, capable of detecting hostile radar emissions at long range. Emitter information is processed by the central mission computer. Detection, identification, direction-finding, and jammer-set-on-sequence may be performed automatically or by the crew. The power plant are two Pratt & Whitney J52-P408 turbofan engines, thrust 11,200 pounds (4,767 kilograms) each. The crew of the Prowler consists of the pilot and three electronic countermeasures officers (ECMOs). The two ECMOs in the aft cockpit operate the ALQ-99 jammers. The ECMO in the right front seat is responsible for navigation, communications, and defensive electronic countermeasures. The EA-6B's ALQ-99 OBS is used to collect tactical electronic order of battle (EOB) data which can be disseminated through the command and control system while airborne. The data can be recorded and processed after missions to provide updates to various orders of battle. The ALQ-00 TJS is used to provide active radar jamming support to aircrtafts, as well as ground units. It may also use HARM to destroy the radar target. The variation of EA-6B include: Basic version, 4 produced; Standard version, 24; ICAP-I, improved jamming ability, 45 produced and all EA-6B turned into this standard before 1983. The current configuration of EA-6B is ICAP-II Block 82, first introduced in 1984, which the Marines have been flying since 1987. The jamming ability is much more improved. Total production of ICAP-II is 72. ICAP-II Block 89A is currently being introduced and will be fully delivered in FY-02. ADVCAP, the newest version. Block2000, the modification of ADVCAP is planned to equip Joint Tactical Information Distribution System, as well as the satellite communication and better viability. The EA-6B will begin retirement in the 2010 timeframe, after a career that exceeded 40 years of deployments in support of USN, USMC, and USAF strike forces. As of early 2000, Defense Department planning for replacing the EA-6B Prowler include a scheme under which the Navy would buy an F/A-18G "Growler" -- an F/A-18E/F modified for escort and close-in jamming. The Air Force would provide standoff jamming with modified EB-52s or EB-1s, and close-in jamming with unmanned air vehicles such as the Northrop Grumman Global Hawk or General Atomics Predator. The unit cost of EA-6B is $52,000,000. In the coming years, the Prowler fleet will be modernized and upgraded to keep the aircraft and its systems abreast of evolving threats and to maintain aircraft safety. The Block 89A upgrade program will address structural and supportability problems associated with aging aircraft and includes numerous avionics improvements for safety of flight and joint interoperability. Later improvements to the Prowler's AN/ALQ-99 tactical jamming system, including the Improved Capabilities (ICAP) III upgrade, new high and low frequency transmitters, and continuing structural enhancements, will ensure that the EA-6B remains the world's premier tactical electronic warfare platform and a force multiplier for years to come. The Marine Corps EA-6B Prowler provides Airborne Command and Control (C2W) support to Fleet Marine Forces to include electronic attack (EA), tactical electronic support (ES), electronic protection (EP) and high speed anti-radiation missile (HARM).
The EA-6B's ALQ-99 OBS is used to collect tactical electronic order of battle (EOB) data which can be disseminated through the command and control system while airborne, and which can be recorded and processed after missions to provide updates to various orders of battle. The ALQ-00 TJS is used to provide active radar jamming support to assault support and attack aircrtaft, as well as ground units. Additional suppression of enemy air defenses (SEAD) capability is available with the employment of HARM. Marine Prowlers may be land-based from prepared airfields, or they can operate from expeditionary airfields (EAF). They may also be sea-based, operating from aircraft carriers. Marine Prowlers are unique in their integration with the Tactical Electronic Processing and Evaluation System (TERPES). TERPES provides post-mission analysis of EA-6B ES data for reporting and updating orders of battle. It also provides post-mission analysis of jamming and HARM employment for reporting, assessing and storing mission data. Following the transition from the EA-6A aircraft to the EA-6B, Marine Tactical Electronic Warfare Squadron 2 (VMAQ-2) continued to provide detachments to Carrier Air Wing Five on board the USS Midway. In 1980 VMAQ-2 completed its assignment aboard the Midway and began shore-based rotations with the 1st Marine Aircraft Wing in Iwakuni, Japan. Detachments were subsequently sent back to sea duty aboard the USS Saratoga and USS America. Marine Prowlers supported joint operations against Libya in 1986 from the carrier. During Operations Desert Storm and Desert Shield VMAQ-2 had one detachment (six aircraft) deployed in Japan and the remainder of the squadron (12 aircraft) deployed to the Persian Gulf. The Reserve squadron, VMAQ-4 (six aircraft), transitioned from the EA-6A to the EA-6B and subsequently relieved the detachment in Japan. During Desert Shield the squadron flew 936 sorties for over 2100 hours. Marine Prowlers flew 495 combat missions totaling 1622 hours, supporting the full spectrum of joint and combined missions. Effective Oct. 1, 1992, the Marine Prowler community reorganized its structure. VMAQS are now structured into four active force squadrons (VMAQ-1, 2, 3, 4). Each squadron now has at least five aircraft. This restructuring provides the flexibility necessary for continuing to support peacetime requirements, as well as the capacity to concurrently assign Marine EA-6B forces to commanders in different areas of operation. One squadron was assigned to Carrier Airwing One on USS America (CV 66) in FY95, while the others continue to support the Unit Deployment Program and CINC contingency requirements. Firing AGM-88. The EA-6B Block 89A is supposed to IOC in 2000. The upgrade promises to be a substantial improvement over previous Block aircraft. The communication system is designed around two ARC-210's in the front and one ARC-182 in the back. In addition to being capable of the same communication frequency ranges as the ARC-182, the ARC-210's also have integrated HAVEQUICK and SINCGARS functions. Another really nice feature about the ARC-210's is that they are integrated with the control display navigation unit (CDNU) so that you can control the radios (all three of them) from a "Radio" page on the CDNU. Navigation system upgrades are also very substantial. The primary navigation sensor is the Litton CN-1649(V)4/ASN-172 Embedded GPS/INS (EGI). This unit combines the Litton LN-100G strapdown inertial unit with a GPS receiver. The result is that the system, or the aircrew, can select from four possible navigation solutions from this one unit. You can select a pure inertial, GPS, filtered inertial, or filtered inertial solution with GPS aiding. Most of the testing used the filtered inertial solution with GPS aiding, called Blended/Coupled, because it was typically the most accurate. This mode allowed the Prowler to navigate with an accuracy of about 16 m (52 ft), a big improvement! The ASN-130 is still in the aircraft as the secondary attitude and navigation source with all the capability it has always had. The 89A also features an improved databus structure that allows the CDNU to integrate many things like the radios, RADAR cursor, both navigation sensors, route control, HARM control, WRA BIT, and current navigation and attitude information. Software improvements to the AGM-88 High-Speed Antiradiation Missile (HARM) have created the Block IIIA and V missile from the Block III and IV hardware. To ensure continued EA-6B compatibility, OFP's SSA 5.2 and 89A 1.0 have been developed by the Weapons System Support Activity, Point Mugu, California. Both are baselined from 5.1 COD, will include HARM III/IIIA/IV/V, and are supported by the same TEAMS release. Two successful live fires of IIIA and V missiles from Block 89A aircraft were made in September 1998 and will be followed this winter by Block 82/89 live fires. The differences in the OFP software will be nearly transparent to the fleet when Block 89A's start arriving. The 89A 1.0 OFP has been optimized for the Block 89A avionics architecture that includes a second 1553 navigation bus and CDNU bus control. The flip side of the new capabilities is that both the MATT and IDM are controlled using a commercially ruggedized laptop computer in a Windows 95 environment, connected by a cable to the center console in the rear cockpit. This less-than-optimum solution of system engineering will be solved when both MATT and IDM systems are integrated into the aircraft displays on the future ICAP III model of the EA-6B. The USQ-113(V)3 Radio Countermeasures Set, also known as Phase III, was designed to detect, analyze, monitor, and/or jam voice and data link signals. Block 89 has undergone extensive ground testing for the USQ-113, following resumption of testing in September 1998. Ground testing was stopped due to software immaturity and BIT reliability problems. Anechoic chamber testing included finishing electromagnetic compatibility, TEMPEST, precipitation-static, and system performance. Electromagnetic vulnerability testing took place in mid February 1999, and flight testing began at the end of the month. The USQ-113 is controlled primarily by the same ruggedized laptop computer that is used for the MATT/IDM systems, or by an improved operator control panel in the front cockpit. The dual seat EA-6A. EA-6B Length: 59 feet (17.98 meters) |