David
Wed December 11, 2002 3:44pm
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The allies dropped large
The allies dropped large amounts of forged rationing cards over Germany These ranged from forged clothing ration books to many types of food rationing cards. The aim of these documents was to disrupt the internal distribution (economic sabotage) by dropping large amounts of them over German civilians. But in at least one German report, there is a mentioning of forged clothing ration books found in crashed aircraft. It was supposed by the Germans that these documents were to help British aircrew in getting access to civilian clothing.
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David
Thu December 19, 2002 2:35pm
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Staff Sgt. Neal Lucero (l
Staff Sgt. Neal Lucero (left) and Staff Sgt. Lee Archuleta review documents for a cargo discharge at an operating location in support of the U.S. Central Command execution of Operation Enduring Freedom. The two review documents associated with the discharge of the vessel Cornhusker. The soldiers are members of the U.S. Army's 599th Transportation Group, Military Traffic Management Command. Training for the mission began in October when many seasoned 599th Group workers assembled in Yokohama for a two-week intensive deployment support team train-up and mission rehearsal. The training was specifically designed to prepare for a possible deployment in support of Enduring Freedom.
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David
Fri December 20, 2002 9:47pm
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Photographer
Photographer?s Mate 2nd Class John Beeman photographically documents an underway replenishment (UNREP), as the Military Sealift Command auxiliary combat stores ship USNS Spica (T-AFS 9) approaches the Truman. Underway Replenishment is the method by which provisions, ammunition and fuel are transferred from one ship to another at sea. The technique enables a fleet or naval formation to remain at sea for prolonged periods of time. Harry S. Truman is on a regularly scheduled deployment, conducting missions in support of Operation Enduring Freedom. U.S. Navy photo by Photographer's Mate 3rd Class Christopher B. Stoltz.
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David
Fri December 20, 2002 9:47pm
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Photographer's Mate 3rd C
Photographer's Mate 3rd Class Jason P. Taylor documents replenishment at sea operations while the Military Sealift Command ship USNS Laramie (T-AO 203) provides Truman with jet fuel for future flight operations. Truman is conducting carrier qualifications off the East coast of the United States. U.S. Navy photo by Photographer's Mate 3rd Class Justin Bane.
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David
Thu January 16, 2003 10:39am
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CH-47 Chinook
Function: Fire support and security for forward and rear area forces, point target/anti-armor, anti-helicopter, armed escort, supporting arms control and coordination, point and limited area air defense from enemy fixed-wing aircraft, armed and visual reconnaissance.
History: Development of the medium lift Boeing Vertol (models 114 and 414) CH-47 Series Chinook began in 1956. Since then the effectiveness of the Chinook has been continually upgraded by successive product improvements, the CH-47A, CH-47B, CH-47C, and CH-47D. The amount of load a cargo helicopter can carry depends on the model, the fuel on board, the distance to be flown, and atmospheric conditions.
The CH-47B was introduced by Boeing after a production run of over 350 CH-47A?s . The B model introduced the Lycoming T55-L7C engine, a beefed up airframe. Nonsymmetrical rotor blades, and the blunted aft pylon for better stability. Boeing began delivering the CH-47B in May of 1967 and eventually produced a total of 108 B models before production shifted to the CH-47C.
During Desert Storm the CH-47D was often the only mode of transportation to shift large numbers of personnel, equipment, and supplies rapidly over the vast area in which US forces operated. The cargo capacity and speed provided commanders and logisticians a capability unequalled by any Army in the world." (Army Aviation in Operation Desert Storm, 1991) During the ground phase, the flanking maneuver executed by the XVIII Airborne Corps was planned with the CH-47D as the keystone. Forward Operating Base Cobra was deliberately positioned to accommodate the combat radius of a fully loaded CH-47D. Cobra was initially secured by an air assault of the 101st's 2nd Infantry Brigade. This air assault, consisting of 5000 soldiers, was accomplished by a total of 126 Blackhawks and 60 Chinooks. By the end of the first day the CH-47Ds had lifted 131,000 gallons of fuel along with pallets of combat-configured ammunition for the next day's fight. Forty separate refueling and rearming points were active in FOB Cobra in less than two hours.
During peacekeeping operations in Bosnia, a Chinook company (A company, 5th Battalion, 159th Aviation Regiment) of 16 aircraft flew 2,222 hours, carried 3,348 passengers, and transported over 3.2 million pounds of cargo over a six month period. These numbers equate to carrying 112 infantry platoons, 545 HMMWVs, or 201 M198 Howitzers. The most publicized mission was assisting the 502d Engineer Company build a float bridge across the flooded Sava River allowing the 1st Armored Division to cross into Bosnia. On 29 and 30 December 1995, Big Windy lifted bridge bays and dropped them into the Sava River so the engineers could quickly assemble the bridge. When the Sava River flood washed away the engineer's tentage and personal equipment, Big Windy quickly resupplied the engineers so they could continue their vital mission. Additionally, a key early mission in support of NATO was the recovery of Admiral Smith's aircraft. The Blackhawk had performed a precautionary landing for what was later found to be a transmission seizure. A CH-47D sling-loaded the Blackhawk back to the Intermediate Staging Base (ISB). Big Windy began redeploying to Giebelstadt on 14 June 1996. One platoon of six CH-47Ds remained in Hungary throughout 1997.
Description: The CH-47 is a twin-engine, tandem rotor helicopter designed for transportation of cargo, troops, and weapons during day, night, visual, and instrument conditions. The aircraft fuselage is approximately 50 feet long. With a 60-foot rotor span, on each rotor system, the effective length of a CH-47 (with blades turning) is approximately 100 feet from the most forward point of the forward rotor to the most rearward point on the aft rotor. Maximum airspeed is 170 knots with a normal cruise speed of 130 knots. However, speed for any mission will vary greatly depending on load configuration (internal or external), time of day, or weather conditions. The minimum crew for tactical operations is four, two pilots, one flight engineer, and one crew chief. For more complex missions, such as NVG operations and air assaults, commanders may consider using five crew members and add one additional crew chief.
The CH-47A, first delivered for use in Vietnam in 1962, is a tandem-rotor medium transport helicopter. The Chinook's primary mission is moving artillery, ammunition, personnel, amd supplies on the battlefield. It also performs rescue, aeromedical, parachuting, aircraft recovery and special operations missions. On June 25, 1958 the Army issued an invitation for a General Management Proposal for the US Army Medium Transport Helicopter. Five aircraft selected Vertol to produce the YCH-1B as the Army?s new medium transport helicopter. In July 1962 DoD redesignated all U.S. military aircraft and the HC-1B was redesignated the as the CH-47A. Early production CH-47A?s operated with the 11th Air Assault Division during 1963 and in October of that year the aircraft was formally designated as the Army?s standard medium transport helicopter. In June 1965 the 11th Air Assault Division was redesignated as the 1st Cavalry Division (Airmobile) and readied for deployment to Viet Nam. Chinooks from the 11th Air Assault formed the nucleus of the 228th Assault Helicopter Battalion which began operations in Viet Nam in September, 1965. CH-47A?s deployed to Viet Nam were equipped with Lycoming T55-L7 engines generating 2650 shp. The aircraft had a maximum gross weight of 33,000 pounds allowing for a maximum payload of approximately 10,000 pounds. The hot mountainous conditions of Viet Nam limited the A models performance capabilities and generated a requirement for increased payload and better performance.
The CH-47C Chinook model has a maximum cargo hook capacity of 20,000 pounds. The CH-47C has only a single cargo hook below the center of the aircraft. When hooking a single load, soldiers use the main hook. They must coordinate closely with the aircrew as to which hooks to use when carrying multiple loads. The planning figure for the fore and aft hooks is 10,000 pounds each. The Army?s continued need for further performance improvements lead to the development of the CH-47C. Designed to meet an Army requirement to transport a 15,000 pound sling load over a 30 mile radius, the C model boasted an increased gross weight to 46,000 pounds, increased fuel capacity, the Lycoming T55-L11 engine developing 3750 shp, and addition structural improvements. The first C model flew in late 1967 and became the mainstay of the Chinook fleet until the advent of the CH-47D. Production of the C model continued until 1980 with improvements such as the crash worthy fuel system and fiberglass rotor blades being incorporated into the fleet.
The CH-47D was the result of June 1976 contract for a modernized Chinook. The Army recognized that that the Chinook fleet was rapidly reaching the end of its useful life and signed a contract with Boeing to significantly improve and update the CH-47. Three airframes, CH-47A, CH-47B, and a CH-47C, were stripped down to their basic airframes and then rebuilt with improved systems to provide three CH-47D prototypes. Improvements included upgraded power plants, rotor transmissions, integral lubrication and cooling for the transmission systems, and fiberglass rotor blades. Other improvements included a redesigned cockpit to reduce pilot workload, redundant and improved electrical systems, modularized hydraulic systems, an advanced flight control system, and improved avionics. The Chinook has two tandem three-bladed counter-rotating fiberglass rotors. The CH-47D is powered by two Allied Signal Engines T55-L-712 3750 shp turboshaft engines and has a maximun speed of 163 mph (142 knots). The CH-47D was rolled-out in March 1979. The CH-47D carrys twice the load of a CH-47A and has improved performance. The CH-47D can operate at night and in nearly all weather conditions. The CH-47D is equipped with an air-to-air refueling probe. The Chinook can accommodate a wide variety of internal payloads, including vehicles, artillery pieces, 33 to 44 troops, or 24 litters plus two medical attendants. The Chinook can be equipped with two door mounting M60D 7.62mm machine guns on the M24 armament subsystem and a ramp mounting M60D using the M41 armament subsystem. The "D" model can carry up to 26,000 pounds externally. The CH-47D has three cargo hooks: a center (main) hook and two additional hooks fore and aft of the main hook.
The Fatcow is a CH-47 with the Extended Range Fuel System [ERFS] II system located in the cargo bay. The configuration consists of three or four fuel tanks attached to a refueling system. The system contains 2400 gallons of JP4/8 excluding the CH-47 internal fuel load of 1050 gals. The Fatcow can set up a 1,2,3,or 4 point system using HTARS. The fuel cells must be crash-worthy and self sealing up to 50 caliber hits.
The Improved Cargo Helicopter (ICH) is a remanufactured version of the CH-47D Chinook cargo helicopter with the new T55-GA-714A engines. The ICH program is intended to restore CH-47D airframes to their original condition and extend the aircraft's life expectancy another 20 years (total life of 60 years) until the 2025-2030 timeframe. The program will remanufacture CH-47 aircraft, reduce the aircraft's vibration, thereby reducing Operations and Support costs, and allow the aircraft to operate on the digitized battlefield by incorporating a 1553 data bus. The ICH will also acquire the capability to carry 16,000 pounds of external/internal cargo for a 50 NM combat radius at 4000 feet pressure altitude and 95 degrees fahrenheit. In addition, the following improvements will be incorporated into the aircraft:
- Fuselage stiffening and possible active systems for vibration reduction (this is expected to lead to improved reliability and therefore reduced operating and support costs)
- Integrated cockpit
- Digital architecture for Force XXI compatibility
Additional improvements may be incorporated into the aircraft if funding permits. The ICH will transport weapons, ammunition, equipment, troops, and other cargo in general support of combat units and operations other than war. The ICH is a dominant maneuver platform that provides focused logistics to the force. The ICH program was built as a "bare bones" program to satisfy the battlefield requirements of operations on the 21st century digital battlefield by replacing the existing 1970s technology cockpit with a new cockpit.
The 101st Air Assault Division is scheduled to receive the first ICH in FY03. The First Unit Equipped (FUE) date to the 101st, a company of sixteen aircraft, is FY04. The 101st, 18th Airborne Corps, Korea, and USAREUR will complete fielding through FY09. ICH completes the fielding of 300 aircraft in 2015. Only 300 of the 431 CH-47Ds convert to ICHs based on the fielding of JTR. As the Army fields JTR to Force Package One units, the ICH aircraft will cascade to units that retained CH-47Ds. Those CH-47Ds would retire.
Separate programmatically from the ICH program, the 714 engine program is an Engineering Change Proposal (ECP) to convert the present T-55-712 engines to a T-55-714 engine. This buys back performance on high/hot days lost over time by the addition of weight through modification work order enhancements. Specifically, it will provide an increased lift capability allowing the CH-47 to transport 16,000 pounds for an unrefueled combat radius of 50 nautical miles at 4,000 feet PA and 95 degrees F. The ICH Operational Requirements Document (ORD) requires the CH-47F(ICH) to carry 16,000lbs at 4000ft/95? for a 50nm combat radius (50nm with load, return empty). The CH-47D -714A engine program achieves this requirement. The -714A engine program converts current CH-47D -712 engines to -714A engines. The engine program converts the engines on all 431 CH-47D aircraft. The -714A engine begins fielding in FY99 and, because of recent budget cuts, completes in FY09. 160th (Hunter), 101st, 18th AB Corps, Korea, and Germany are scheduled to be fielded through FY05. The -714A budget constantly fluctuates because of plus-ups and decrements. For this reason, the fielding dates may change.
The MH-47E Special Operations Aircraft (SOA) is a derivative of the Boeing CH-47 Chinook. Included with other modifications is a significantly increased fuel capacity with modified main and auxiliary fuel tanks. The aircraft has modified integrated avionics suites and multi-mode radars and is intended to provide adverse-weather infiltration/exfiltration and support to US Military Forces, country teams, other agencies and special activities. The CH-47D Chinook has been specially modified to perform the special operations mission and has been tested in combat. The three versions of the CH-47 in the Army inventory are the CH-47D, the MH-47D, and the MH-47E. The MH-47D and the MH-47E are air refuelable. It provides long-range penetration, medium assault helicopter support to special operations forces. Depending on the version, it can be ferried 1,100 to 2,000 nautical miles unrefueled. During Operation Just Cause, CH-47s conducted H-hour assaults to support other elements who were air-landing SOF to disrupt enemy responses and seize key facilities. During Operation Desert Storm, the CH-47 conducted infiltration and exfiltration of SOF and CSAR of downed pilots. MH-47E testing was limited to the major change to the aircraft which affects vulnerability. In the case of the MH-47E, this was the addition of an 800 gallon Robertson Auxiliary Fuel Tank in the cabin and Boeing designed sponson tanks with expanded capacity and honeycomb shell construction. Analyses conducted during the test planning phase revealed that the largest potential vulnerability was associated with projectiles entering the fuel tanks in the volume above the liquid fuel. Such impacts could ignite the fuel vapors and cause explosions and/or fires with serious consequences. During test planning, USSOCOM decided to add an inerting system to the fuel tanks to avoid such fires/explosions. This will be a lead-the-fleet system that will be available for similar helicopter variants in other fleets as well.
General Characteristics, CH-47 Chinook
Manufacturer:
Boeing Company
Power Plant:
Two Textron Lycoming T55-L712 engines
Length:
99 feet (30.18 meters), including rotor lengths
Height:
19 feet (5.79 meters)
Rotor Diameter:
60 feet (18.29 meters)
Weight:
Empty: 10,578 kilograms
Maximum: 24,494 kilograms
Useful load: 13,916 kilograms
Forward and aft cargo hooks: 9,072 kilograms
Centre cargo hook 12,701 kilograms
Speed:
Sea level cruise speed: 265 kmh
Speed at maximum continuous power: 269 kmh
Ceiling:
8,448 feet (2,575 meters)
Range:
230 nautical miles
Crew:
Two
Sensors:
Raytheon AN/APQ-174A for terrain following flight, air-to-ground ranging and ground mapping
Raytheon AN/AAQ-16 forward looking infrared (FLIR)
Introduction Date:
1963
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David
Thu January 16, 2003 10:39am
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UH-60 Blackhawk
Description: The Black Hawk is the Army?s front-line utility helicopter used for air assault, air cavalry, and aeromedical evacuation units. It is designed to carry 11 combat-loaded, air assault troops, and it is capable of moving a 105-millimeter howitzer and 30 rounds of ammunition. First deployed in 1978, the Black Hawk?s advanced technology makes it easy to maintain in the field. The Black Hawk has performed admirably in a variety of missions, including air assault, air cavalry and aeromedical evacuations. In addition, modified Black Hawks operate as command and control, electronic warfare, and special operations platforms.
The Black Hawk is the primary division-level transport helicopter, providing dramatic improvements in troop capacity and cargo lift capability compared to the UH-1 Series "Huey" it replaces. The UH-60A, with a crew of three, can lift an entire 11-man fully-equipped infantry squad in most weather conditions. It can be configured to carry four litters, by removing eight troop seats, in the MedEval role. Both the pilot and co-pilot are provided with armor-protective seats. Protective armor on the Black Hawk can withstand hits from 23mm shells. The Black Hawk has a cargo hook for external lift missions. The Black Hawk has provisions for door mounting of two M60D 7.62mm machine guns on the M144 armament subsystem, and can disperse chaff and infrared jamming flares using the M130 general purpose dispenser. The Black Hawk has a composite titanium and fiberglass four-bladed main rotor, is powered by two General Electric T700-GE-700 1622 shp turboshaft engines, and has a speed of 163 mph (142 knots).
Elements of the U.S. Army Aviation UH-60A/l Blackhawk helicopter fleet will begin reaching their sevice life goal of 25 years in 2002. In order for the fleet to remain operationally effective through the time period 2025-2030 the aircraft will need to go through an inspection, refurbishment, and modernization process that will validate the structural integrity of the airframe, incorporate improvements in sub-systems so as to reduce maintenance requirements, and modernize the mission equipment and avionics to the levels compatible with Force XXI and Army After Next (AAN) demands.
A Service Life Extension Program (SLEP) is planned for the UH-60 beginning in FY99. The UH-60 modernization program will identify material requirements to effectively address known operational deficiencies to ensure the Black Hawk is equipped and capable of meeting battlefield requirements through the 2025-2030 timeframe. Primary modernization areas for consideration are: increased lift, advanced avionics (digital communications and navigation suites), enhanced aircraft survivability equipment (ASE), increased reliability and maintainability (R & M), airframe service life extension (SLEP), and reduced operations and support (O & S) costs. Suspense date for the approved Operational Requirements Document (ORD) is December 1998.
History: The UH-60A, first flown in October 1974, was developed as a result of the Utility Tactical Transport Aircraft System (UTTAS) program. The UTTAS was designed for troop transport, command and control, MedEvac, and reconnaissance, to replace the UH-1 Series "Huey" in the combat assault role. In August 1972, the U.S. Army selected the Sikorsky (model S-70) YUH-60A and the Boeing Vertol (model 237) YUH-61A (1974) as competitors in the Utility Tactical Transport Aircraft System (UTTAS) program. The Boeing Vertol YUH-61A had a four-bladed composite rotor, was powered by the same General Electric T700 engine as the Sikorsky YUH-60A, and could carry 11 troops. In December 1976 Sikorsky won the competition to produce the UH-60A, subsequently named the Black Hawk.
Variants: The Army began fielding the UH-60 in 1978. From 1978 until 1989 the Army procured UH-60A model aircraft. In October 1989, a power train upgrade resulted in a model designation change from UH-60A to UH-60L. The UH-60L version that provides 24 percent more power than the original 1970 UH-60A model. As of the end of FY97, the Army had procured 483 UH-60L models for a total UH-60 acquisition of 1,463 aircraft. The Army is in the fifth and final year of a multi-year procurement contract calling for the delivery of 60 aircraft per year.
UH-60L: In October 1989, the engines were upgraded to two General Electric T700-GE-701C 1890 shp turboshaft engines, and an improved durability gear box was added, resulting in a model designation change from UH-60A to UH-60L. The T700-GE-701C has better high altitude and hot weather performance, greater lifting capacity, and improved corrosion protection.
The UH-60 Firehawk is a Reseach and Development program to provide the UH-60 series helicopter with both a wartime and peacetime fire fighting capability by use of a detachable 1,000 gal. belly tank. Qualification issues include design and testing required to maintain the combat capabilities of the UH-60 Black Hawk and the safe flight envelope of the aircraft with the tank.
The EH-60A Electronic Countermeasures (ECM) variant has a unique external antenna designed to intercept and jam enemy communications. The EH-60E is powered by two General Electric T700-GE-700 1622 shp turboshaft engines.
The EH-60B version has a Stand-Off Target Acquisition System designed to detect the movement of enemy forces on the battlefield and relay the information to a ground station.
UH-60Q Medevac: The UH-60Q MEDEVAC helicopter provides significant enroute patient care enhancements. The UH-60Q provides a 6 patient litter system, on-board oxygen generation, and a medical suction system. UH-60Q is a UH-60A derivative and incorporates approximate UH-60A characteristics. It is simply the best in aeromedical evacuation. Building on the BLACK HAWK's heritage of saving lives in Grenada, Panama, Kuwait and Somalia, the UH-60Q delivers exceptional patient care, increased survivability, longer range, greater speed and added missions capability. For military combatants. War victims. Civilians injured in natural disasters. It has a state-of-the-art medical interior that can accomodate a crew of three and up to six acute care patients. The UH-60Q's leading-edge technology incorporates an improved environmental control system. Cardiac monitoring systems. Oxygen generation, distribution and suction systems. Airway management capability. Provision for stowing IV solutions. And an external electrical rescue hoist. And in addition to extensive immediate care, the UH-60Q can perform all weather terrain battlefield evacuation, combat search and rescue, hospital ship lifeline missions, deep operations support, forward surgical team transport, medical logistics resupply, medical personnel movement, patient regulating, disaster/humanitarian relief, and MAST/HELP state support.
The UH-60Q's medical interior can accomodate three to six acute care patients and their medical attendants. Ergonomic design has maximized the UH-60Q cabin space, placing sophisticated, life-saving instruments and equipment at the fingertips of the medical attendants. A unique platform design allows the interior to transport either six litter of seven ambulatory systems, oxygen distribution and suction systems, airway management capability, and provisions for stowing intravenous solutions. The interior also features these additional capabilities, essentical to providing the highest degree of patient care when every second counts:
- Oxygen Generating Systems
- NVG Compatible Lighting Throughout
- Environmental Control System
- Medical Equipment
- Patient Monitoring Equipment
- Neonatal Isolettes
Modernizing the Medical Evacuation (MEDEVAC) system is the Army Surgeon General's number one near term priority. The UH-60Q communications architecture provides situational awareness and digital communications and is expected to be the model for anticipated fleet-wide improvements to the UH-60. Other improvements include integrated Doppler/GPS, Personnel Locator System, NVG interior lighting, and FLIR.
General Characteristics, UH-60 Black Hawk
Contractor:
Sikorsky
Power Plant:
Two T700-GE-701Cs
Thrust:
3,120 shaft horsepower
Length:
64 feet, 7 inches (19.7 meters)
Height:
16 feet, 10 inches
Main Rotor Diameter:
53 feet, 6 inches (16.3 meters)
Weight:
11,500 pounds
External Cargo Hook:
Handles up to 8000 pounds (3629 kilograms)
Maximum Speed:
150 knots
Ceiling:
19,000 feet (5,790 meters)
Range:
315 nautical miles
Crew:
Two pilots and two crew; 11 to 14 armed troops
Armament:
Up to two 7.62mm M60 machine guns in cabin
Two 7.62-mm (0.3-in) miniguns or two GECAL 0.50-in Gatling guns on pintle mount
Date Deployed:
1978
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David
Thu January 16, 2003 6:05pm
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AV-8B Harrier II
Function: The mission of the VMA STOVL squadron is to attack and destroy surface and air targets, to escort helicopters, and to conduct other such air operations as may be directed. Specific tasks of the AV-8B HARRIER II include:
- Conduct close air support using conventional and specific weapons.
- Conduct deep air support, to include armed reconnaissance and air interdiction, using conventional and specific weapons.
- Conduct offensive and defensive antiair warfare. This includes combat air patrol, armed escort missions, and offensive missions against enemy ground-to-air defenses, all within the capabilities of the aircraft.
- Be able to operate and deliver ordnance at night and to operate under instrument flight conditions.
- Be able to deploy for extended operations employing aerial refueling.
- Be able to deploy to and operate from carriers and other suitable seagoing platforms, advanced bases, expeditionary airfields, and remote tactical landing sites.
History: Operation Desert Storm in 1991 was highlighted by expeditionary air operations performed by the AV-8B. The Harrier II was the first Marine Corps tactical strike platform to arrive in theater, and subsequently operated from various basing postures. Three squadrons, totaling 60 aircraft, and one six-aircraft detachment operated ashore from an expeditionary airfield, while one squadron of 20 aircraft operated from a sea platform. During the ground war, AV-8Bs were based as close as 35 nautical miles (40.22 miles) from the Kuwait border, making them the most forward deployed tactical strike aircraft in theater. The AV-8B flew 3,380 sorties for a total of 4,083 flight hours while maintaining a mission capable rate in excess of 90 percent. Average turnaround time during the ground war surge rate flight operations was 23 minutes.
Description: The AV-8B V/STOL strike aircraft was designed to replace the AV-8A and the A-4M light attack aircraft. The Marine Corps requirement for a V/STOL light attack force has been well documented since the late 1950s. Combining tactical mobility, responsiveness, reduced operating cost and basing flexibility, both afloat and ashore, V/STOL aircraft are particularly well-suited to the special combat and expeditionary requirements of the Marine Corps. The AV-8BII+ features the APG-65 Radar common to the F/A-18, as well as all previous systems and features common to the AV-8BII.
?General Characteristics, AV-8B Harrier II
Manufacturer:
McDonnell Douglas
Unit Cost:
$23,700,000
Power Plant:
One Rolls Royce F402-RR-406 or F402-RR-408 turbofan engine
Thrust:
F402-RR-406: 21,500 pounds
F402-44-208: 23,400 pounds
Length:
46.3 feet (14.11 meters)
Wingspan:
30.3 feet (9.24 meters)
Maximum Take-off Weight:
155,000 pounds (69,750 kilograms)
Cruise Speed:
Subsonic to transonic
Ceiling:
25,000 feet (7,576 meters)
Combat Radius:
Close air support: 163 nautical miles (187.45 miles) with 30 minutes time on station
Interdiction: 454 nautical miles (522.45 miles)
Ferry Range:
2100 nautical miles (2416.64 miles)
Armament:
Seven external store stations, comprising six wing stations for AIM-9 Sidewinder and an assortment of air-to-ground weapons, external fuel tanks and AGM-65 Maverick missiles
One centerline station for DECM pod or air-to-ground ordnance; a GAU-12 25MM six-barrel gun pod can be mounted on the centerline and has a 300 round capacity with a lead computing optical sight system (LCOSS) gunsight
Crew:
One
Inventory:
Seven squadrons with 20 aircraft each and one training squadron with 20 AV-8B and 15 TAV-8B aircraft for a total of 175 aircraft
Introduction Date:
January 12, 1985
AV-8BII(Plus) introduced in June 1993
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David
Fri March 21, 2003 6:49am
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Patriot PAC-3 ERINT
Patriot Advanced Capability-3 (PAC-3) is a high/medium advanced surface-to-air guided missile air defense system. PAC-3 is a major upgrade to the Patriot system. The PAC-3 Operational Requirements Document (ORD) represents the Army Air Defense need to buy back required battlespace lost against the current and evolving tactical missile and air breathing threat. PAC-3 is needed to ounter/defeat/destroy the 2008 threat and to extend Patriot's capabilities to accomplish new/revised missions. In tandem with the upgraded radar and ground control station, PAC-3 interceptors can protect an area about seven times greater than the original Patriot system.
The PAC-3 Program consists of two interrelated acquisition programs - The PAC-3 Growth Program and the PAC-3 Missile Program. The Growth program consists of integrated, complementary improvements that will be implemented by a series of phased, incrementally fielded material changes. The PAC-3 Missile program is a key component of the overall improvements of the Patriot system, it will provide essential increases in battlespace, accuracy, and kill potential.
PAC-3 is a much more capable derivative of the PAC-2/GEM system in terms of both coverage and lethality. The PAC-3 has a new interceptor missile with a different kill mechanism--rather than having an exploding warhead, it is a hit-to-kill system. The PAC-3 missile is a smaller and highly efficient missile. The canister is approximately the same size as a PAC-2 canister but contains four missiles and tubes instead of a single round. Selected Patriot launching stations will be modified to accept PAC-3 canisters.
The Battalion Tactical Operations Center (BTOC) is an M900 series 5-ton expandable van that has been modified by the addition of data processing and display equipment, and utilized by the battalion staff to command and control the Patriot battalion. The BTOC allows the staff to perform automated tactical planning, communications link planning, and to display situational awareness information.
In the 1997 budget DOD added about $230 million for the PAC-3 through the Future Years Defense Program (FYDP) and established a realistic schedule to lower the program execution risk by extending the engineering and manufacturing development (EMD) phase of the program by ten months. System performance will be improved by re-phasing the missile and radar procurements; upgrading three launchers per battery with Enhanced Launcher Electronics Systems; and extending the battery's remote launch capability. PAC-3 Low-Rate Initial Production (LRIP) will begin in the second quarter of fiscal year 1998, and the First Unit Equipped (FUE) date is planned for the fourth quarter of fiscal year 1999. The FUE capability will consist of 16 missiles and five radars which will be placed in one battalion. As of 1996, in addition to funds being programmed for the Ballistic Missile Defense Organization, the Army planned to spend $9.6 billion for all planned purchases of Patriot missiles, $490 million for modifications and $335 million for product improvements.
The Patriot Advanced Capability 3 (PAC-3) Initial Operational Test and Evaluation (IOTE) began in 2002. The two major objectives of the Initial Operational Test and Evaluation (IOTE) are: (1) To assess the improvements in system performance provided by modifications in terms of operational effectiveness, suitability, and survivability; (2) to verify that modifications do not degrade the existing capabilities. The Initial Operational Test and Evaluation (IOTE) will be the first operational integration and assessment of the complete Patriot Advanced Capability 3 (PAC-3) Configuration 3 system.
The 2nd Battalion 43rd Air Defense Artillery/108th Air Defense Artillery Brigade serves as the test unit for the Initial Operational Test and Evaluation (IOTE). The unit is equipped with the complete package of Patriot Advanced Capability 3 (PAC-3) Configuration 3 hardware, PDB-5+ software and the Patriot Advanced Capability 3 (PAC-3) missile. The Patriot Project Office has issued the upgraded equipment to 2-43 Air Defense Artillery. 2-43 has completed New Equipment Training (NET) and supports testing necessary to obtain material release of the Patriot Advanced Capability 3 (PAC-3) Missile equipment.
The Initial Operational Test and Evaluation (IOTE) is conducted in four phases: (1) The Sustained Operations Phase is a five-day deployment to McGregor Range using approved tactics and doctrine. 2-43 Air Defense Artillery will defend against live aircraft in accordance with threat test support package in a simulated combat environment; (2) The Interoperability Phase is a six-day demonstration of the Patriot Advanced Capability 3 (PAC-3) interoperability with current Army and Joint Theater Missile Defense Systems. This phase is conducted using the Joint Common Simulated Missile Defense System Exerciser or actual tactical equipment; (3) The Flight Mission Simulator (FMS) Phase is a 22-day test of simulated air battles. The mobile Flight Mission Simulator (FMS) is a Patriot missile system simulation used to stimulate and evaluate radar performance, engagement decision and weapon assignment (EDWA) processing and test the Patriot Advanced Capability 3 (PAC-3)’s capabilities against a full spectrum of threat targets; (4) The Missile Flight Test Phase consists of four live missile tests conducted at White Sands Missile Range and Kwajalein Missile Range.
The Air Defense Artillery Directorate of the Operational Test Command conducts the planning and execution of the Initial Operational Test and Evaluation (IOTE). Once Initial Operational Test and Evaluation (IOTE) is complete, the Army Evaluation Center prepares the system evaluation report. This report provides input for the Patriot Advanced Capability 3 (PAC-3) missile Milestone III decision (full rate production) and the materiel release for the complete Patriot Advanced Capability 3 (PAC-3) system.
Four PAC-3 operational tests [some involving more than one interceptor launch] between February 2002 and May 2002 resulted in three launch failures, two misses and one hit that failed to destroy the incoming warhead. A malfunctioning radar and software problems led to the misses, and the launch failures resulted from electrical problems.
The Army received the first 16 PAC-3s -- a full launcher load -- in September 2001. The Army is authorized to produce the missiles at a rate of 72 a year, and Congress authorize an increase to 96 per year in fiscal 2003. The plan is to eventually produce 144 a year, leading to a total inventory of 1,159 interceptors. Unable to certify that the PAC-3 interceptor was ready for stepped-up production, in mid-2002 Pentagon put off the decision for at least a year, and planned on further testing once fixes are in place.
By early 2000 the cost of each PAC-3 missile had increased from $1.9 million to over $4 million, and the estimated total program cost had risen from $3.9 billion to $6.9 billion. After design and manufacturing modifications were initiated to control costs, the estimted cost per missile dropped to about $3 million, and as of mid-2002 program officials expected to reduce the unit cost to $2 million.
Initial reports of a successful intercept of a Patriot missile-as-target by a Pac-3 missile on 25 April 2002 have sinced proven to be incorrect. A US Army statement said that subsequent analysis showed that the Pac-3 impacted the target missile but failed to destroy the warhead, so the intercept was unsuccessful. A second Pac-3 in the same test failed to launch. A PAC-3 missile successfully intercepted a target ballistic missile over Kwajalein Atoll on 30 May 2002. A second missile, however, failed to launch for unknown reasons. A failure to launch also occurred in the last test on 25 April. The target was a modified Minuteman missile with a separating reentry vehicle. This was the last test in the Initial Operational Test and Evaluation (IOT&E) program, prior to a Pentagon assessment of PAC-3’s readiness for full-rate production.
As of late October 2002 the Army had taken delivery of 38 PAC-3 missiles, with another 15 due for delivery by December. The military is under contract to receive an additional 126 missiles over the 2003-2004 period. Congress increased the fiscal year 2003 budget request for PAC-3 of 72 missiles by an additional 48 missiles. In late November 2002, DOD approved plans to double PAC-3 monthly production rates, with the number of missiles increasing from four to eight per month after more manufacturing equipment and a second shift of personnel were added. DOD will acquire 108 PAC-3 missiles in FY 2004.
The overall procurement objective of 1,159 PAC-3 missiles remains unchanged. The larger purchases in FY-03 and FY-04 may be offset by lower production in FY-08 and FY-09. Instead of buying 216 missiles in each of those years, DOD would receive 184 units annually.
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David
Fri March 21, 2003 6:49am
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Patriot PAC-3 ERINT
Patriot Advanced Capability-3 (PAC-3) is a high/medium advanced surface-to-air guided missile air defense system. PAC-3 is a major upgrade to the Patriot system. The PAC-3 Operational Requirements Document (ORD) represents the Army Air Defense need to buy back required battlespace lost against the current and evolving tactical missile and air breathing threat. PAC-3 is needed to ounter/defeat/destroy the 2008 threat and to extend Patriot's capabilities to accomplish new/revised missions. In tandem with the upgraded radar and ground control station, PAC-3 interceptors can protect an area about seven times greater than the original Patriot system.
The PAC-3 Program consists of two interrelated acquisition programs - The PAC-3 Growth Program and the PAC-3 Missile Program. The Growth program consists of integrated, complementary improvements that will be implemented by a series of phased, incrementally fielded material changes. The PAC-3 Missile program is a key component of the overall improvements of the Patriot system, it will provide essential increases in battlespace, accuracy, and kill potential.
PAC-3 is a much more capable derivative of the PAC-2/GEM system in terms of both coverage and lethality. The PAC-3 has a new interceptor missile with a different kill mechanism--rather than having an exploding warhead, it is a hit-to-kill system. The PAC-3 missile is a smaller and highly efficient missile. The canister is approximately the same size as a PAC-2 canister but contains four missiles and tubes instead of a single round. Selected Patriot launching stations will be modified to accept PAC-3 canisters.
The Battalion Tactical Operations Center (BTOC) is an M900 series 5-ton expandable van that has been modified by the addition of data processing and display equipment, and utilized by the battalion staff to command and control the Patriot battalion. The BTOC allows the staff to perform automated tactical planning, communications link planning, and to display situational awareness information.
In the 1997 budget DOD added about $230 million for the PAC-3 through the Future Years Defense Program (FYDP) and established a realistic schedule to lower the program execution risk by extending the engineering and manufacturing development (EMD) phase of the program by ten months. System performance will be improved by re-phasing the missile and radar procurements; upgrading three launchers per battery with Enhanced Launcher Electronics Systems; and extending the battery's remote launch capability. PAC-3 Low-Rate Initial Production (LRIP) will begin in the second quarter of fiscal year 1998, and the First Unit Equipped (FUE) date is planned for the fourth quarter of fiscal year 1999. The FUE capability will consist of 16 missiles and five radars which will be placed in one battalion. As of 1996, in addition to funds being programmed for the Ballistic Missile Defense Organization, the Army planned to spend $9.6 billion for all planned purchases of Patriot missiles, $490 million for modifications and $335 million for product improvements.
The Patriot Advanced Capability 3 (PAC-3) Initial Operational Test and Evaluation (IOTE) began in 2002. The two major objectives of the Initial Operational Test and Evaluation (IOTE) are: (1) To assess the improvements in system performance provided by modifications in terms of operational effectiveness, suitability, and survivability; (2) to verify that modifications do not degrade the existing capabilities. The Initial Operational Test and Evaluation (IOTE) will be the first operational integration and assessment of the complete Patriot Advanced Capability 3 (PAC-3) Configuration 3 system.
The 2nd Battalion 43rd Air Defense Artillery/108th Air Defense Artillery Brigade serves as the test unit for the Initial Operational Test and Evaluation (IOTE). The unit is equipped with the complete package of Patriot Advanced Capability 3 (PAC-3) Configuration 3 hardware, PDB-5+ software and the Patriot Advanced Capability 3 (PAC-3) missile. The Patriot Project Office has issued the upgraded equipment to 2-43 Air Defense Artillery. 2-43 has completed New Equipment Training (NET) and supports testing necessary to obtain material release of the Patriot Advanced Capability 3 (PAC-3) Missile equipment.
The Initial Operational Test and Evaluation (IOTE) is conducted in four phases: (1) The Sustained Operations Phase is a five-day deployment to McGregor Range using approved tactics and doctrine. 2-43 Air Defense Artillery will defend against live aircraft in accordance with threat test support package in a simulated combat environment; (2) The Interoperability Phase is a six-day demonstration of the Patriot Advanced Capability 3 (PAC-3) interoperability with current Army and Joint Theater Missile Defense Systems. This phase is conducted using the Joint Common Simulated Missile Defense System Exerciser or actual tactical equipment; (3) The Flight Mission Simulator (FMS) Phase is a 22-day test of simulated air battles. The mobile Flight Mission Simulator (FMS) is a Patriot missile system simulation used to stimulate and evaluate radar performance, engagement decision and weapon assignment (EDWA) processing and test the Patriot Advanced Capability 3 (PAC-3)’s capabilities against a full spectrum of threat targets; (4) The Missile Flight Test Phase consists of four live missile tests conducted at White Sands Missile Range and Kwajalein Missile Range.
The Air Defense Artillery Directorate of the Operational Test Command conducts the planning and execution of the Initial Operational Test and Evaluation (IOTE). Once Initial Operational Test and Evaluation (IOTE) is complete, the Army Evaluation Center prepares the system evaluation report. This report provides input for the Patriot Advanced Capability 3 (PAC-3) missile Milestone III decision (full rate production) and the materiel release for the complete Patriot Advanced Capability 3 (PAC-3) system.
Four PAC-3 operational tests [some involving more than one interceptor launch] between February 2002 and May 2002 resulted in three launch failures, two misses and one hit that failed to destroy the incoming warhead. A malfunctioning radar and software problems led to the misses, and the launch failures resulted from electrical problems.
The Army received the first 16 PAC-3s -- a full launcher load -- in September 2001. The Army is authorized to produce the missiles at a rate of 72 a year, and Congress authorize an increase to 96 per year in fiscal 2003. The plan is to eventually produce 144 a year, leading to a total inventory of 1,159 interceptors. Unable to certify that the PAC-3 interceptor was ready for stepped-up production, in mid-2002 Pentagon put off the decision for at least a year, and planned on further testing once fixes are in place.
By early 2000 the cost of each PAC-3 missile had increased from $1.9 million to over $4 million, and the estimated total program cost had risen from $3.9 billion to $6.9 billion. After design and manufacturing modifications were initiated to control costs, the estimted cost per missile dropped to about $3 million, and as of mid-2002 program officials expected to reduce the unit cost to $2 million.
Initial reports of a successful intercept of a Patriot missile-as-target by a Pac-3 missile on 25 April 2002 have sinced proven to be incorrect. A US Army statement said that subsequent analysis showed that the Pac-3 impacted the target missile but failed to destroy the warhead, so the intercept was unsuccessful. A second Pac-3 in the same test failed to launch. A PAC-3 missile successfully intercepted a target ballistic missile over Kwajalein Atoll on 30 May 2002. A second missile, however, failed to launch for unknown reasons. A failure to launch also occurred in the last test on 25 April. The target was a modified Minuteman missile with a separating reentry vehicle. This was the last test in the Initial Operational Test and Evaluation (IOT&E) program, prior to a Pentagon assessment of PAC-3’s readiness for full-rate production.
As of late October 2002 the Army had taken delivery of 38 PAC-3 missiles, with another 15 due for delivery by December. The military is under contract to receive an additional 126 missiles over the 2003-2004 period. Congress increased the fiscal year 2003 budget request for PAC-3 of 72 missiles by an additional 48 missiles. In late November 2002, DOD approved plans to double PAC-3 monthly production rates, with the number of missiles increasing from four to eight per month after more manufacturing equipment and a second shift of personnel were added. DOD will acquire 108 PAC-3 missiles in FY 2004.
The overall procurement objective of 1,159 PAC-3 missiles remains unchanged. The larger purchases in FY-03 and FY-04 may be offset by lower production in FY-08 and FY-09. Instead of buying 216 missiles in each of those years, DOD would receive 184 units annually.
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David
Fri March 21, 2003 6:49am
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Patriot PAC-3 ERINT
Patriot Advanced Capability-3 (PAC-3) is a high/medium advanced surface-to-air guided missile air defense system. PAC-3 is a major upgrade to the Patriot system. The PAC-3 Operational Requirements Document (ORD) represents the Army Air Defense need to buy back required battlespace lost against the current and evolving tactical missile and air breathing threat. PAC-3 is needed to ounter/defeat/destroy the 2008 threat and to extend Patriot's capabilities to accomplish new/revised missions. In tandem with the upgraded radar and ground control station, PAC-3 interceptors can protect an area about seven times greater than the original Patriot system.
The PAC-3 Program consists of two interrelated acquisition programs - The PAC-3 Growth Program and the PAC-3 Missile Program. The Growth program consists of integrated, complementary improvements that will be implemented by a series of phased, incrementally fielded material changes. The PAC-3 Missile program is a key component of the overall improvements of the Patriot system, it will provide essential increases in battlespace, accuracy, and kill potential.
PAC-3 is a much more capable derivative of the PAC-2/GEM system in terms of both coverage and lethality. The PAC-3 has a new interceptor missile with a different kill mechanism--rather than having an exploding warhead, it is a hit-to-kill system. The PAC-3 missile is a smaller and highly efficient missile. The canister is approximately the same size as a PAC-2 canister but contains four missiles and tubes instead of a single round. Selected Patriot launching stations will be modified to accept PAC-3 canisters.
The Battalion Tactical Operations Center (BTOC) is an M900 series 5-ton expandable van that has been modified by the addition of data processing and display equipment, and utilized by the battalion staff to command and control the Patriot battalion. The BTOC allows the staff to perform automated tactical planning, communications link planning, and to display situational awareness information.
In the 1997 budget DOD added about $230 million for the PAC-3 through the Future Years Defense Program (FYDP) and established a realistic schedule to lower the program execution risk by extending the engineering and manufacturing development (EMD) phase of the program by ten months. System performance will be improved by re-phasing the missile and radar procurements; upgrading three launchers per battery with Enhanced Launcher Electronics Systems; and extending the battery's remote launch capability. PAC-3 Low-Rate Initial Production (LRIP) will begin in the second quarter of fiscal year 1998, and the First Unit Equipped (FUE) date is planned for the fourth quarter of fiscal year 1999. The FUE capability will consist of 16 missiles and five radars which will be placed in one battalion. As of 1996, in addition to funds being programmed for the Ballistic Missile Defense Organization, the Army planned to spend $9.6 billion for all planned purchases of Patriot missiles, $490 million for modifications and $335 million for product improvements.
The Patriot Advanced Capability 3 (PAC-3) Initial Operational Test and Evaluation (IOTE) began in 2002. The two major objectives of the Initial Operational Test and Evaluation (IOTE) are: (1) To assess the improvements in system performance provided by modifications in terms of operational effectiveness, suitability, and survivability; (2) to verify that modifications do not degrade the existing capabilities. The Initial Operational Test and Evaluation (IOTE) will be the first operational integration and assessment of the complete Patriot Advanced Capability 3 (PAC-3) Configuration 3 system.
The 2nd Battalion 43rd Air Defense Artillery/108th Air Defense Artillery Brigade serves as the test unit for the Initial Operational Test and Evaluation (IOTE). The unit is equipped with the complete package of Patriot Advanced Capability 3 (PAC-3) Configuration 3 hardware, PDB-5+ software and the Patriot Advanced Capability 3 (PAC-3) missile. The Patriot Project Office has issued the upgraded equipment to 2-43 Air Defense Artillery. 2-43 has completed New Equipment Training (NET) and supports testing necessary to obtain material release of the Patriot Advanced Capability 3 (PAC-3) Missile equipment.
The Initial Operational Test and Evaluation (IOTE) is conducted in four phases: (1) The Sustained Operations Phase is a five-day deployment to McGregor Range using approved tactics and doctrine. 2-43 Air Defense Artillery will defend against live aircraft in accordance with threat test support package in a simulated combat environment; (2) The Interoperability Phase is a six-day demonstration of the Patriot Advanced Capability 3 (PAC-3) interoperability with current Army and Joint Theater Missile Defense Systems. This phase is conducted using the Joint Common Simulated Missile Defense System Exerciser or actual tactical equipment; (3) The Flight Mission Simulator (FMS) Phase is a 22-day test of simulated air battles. The mobile Flight Mission Simulator (FMS) is a Patriot missile system simulation used to stimulate and evaluate radar performance, engagement decision and weapon assignment (EDWA) processing and test the Patriot Advanced Capability 3 (PAC-3)’s capabilities against a full spectrum of threat targets; (4) The Missile Flight Test Phase consists of four live missile tests conducted at White Sands Missile Range and Kwajalein Missile Range.
The Air Defense Artillery Directorate of the Operational Test Command conducts the planning and execution of the Initial Operational Test and Evaluation (IOTE). Once Initial Operational Test and Evaluation (IOTE) is complete, the Army Evaluation Center prepares the system evaluation report. This report provides input for the Patriot Advanced Capability 3 (PAC-3) missile Milestone III decision (full rate production) and the materiel release for the complete Patriot Advanced Capability 3 (PAC-3) system.
Four PAC-3 operational tests [some involving more than one interceptor launch] between February 2002 and May 2002 resulted in three launch failures, two misses and one hit that failed to destroy the incoming warhead. A malfunctioning radar and software problems led to the misses, and the launch failures resulted from electrical problems.
The Army received the first 16 PAC-3s -- a full launcher load -- in September 2001. The Army is authorized to produce the missiles at a rate of 72 a year, and Congress authorize an increase to 96 per year in fiscal 2003. The plan is to eventually produce 144 a year, leading to a total inventory of 1,159 interceptors. Unable to certify that the PAC-3 interceptor was ready for stepped-up production, in mid-2002 Pentagon put off the decision for at least a year, and planned on further testing once fixes are in place.
By early 2000 the cost of each PAC-3 missile had increased from $1.9 million to over $4 million, and the estimated total program cost had risen from $3.9 billion to $6.9 billion. After design and manufacturing modifications were initiated to control costs, the estimted cost per missile dropped to about $3 million, and as of mid-2002 program officials expected to reduce the unit cost to $2 million.
Initial reports of a successful intercept of a Patriot missile-as-target by a Pac-3 missile on 25 April 2002 have sinced proven to be incorrect. A US Army statement said that subsequent analysis showed that the Pac-3 impacted the target missile but failed to destroy the warhead, so the intercept was unsuccessful. A second Pac-3 in the same test failed to launch. A PAC-3 missile successfully intercepted a target ballistic missile over Kwajalein Atoll on 30 May 2002. A second missile, however, failed to launch for unknown reasons. A failure to launch also occurred in the last test on 25 April. The target was a modified Minuteman missile with a separating reentry vehicle. This was the last test in the Initial Operational Test and Evaluation (IOT&E) program, prior to a Pentagon assessment of PAC-3’s readiness for full-rate production.
As of late October 2002 the Army had taken delivery of 38 PAC-3 missiles, with another 15 due for delivery by December. The military is under contract to receive an additional 126 missiles over the 2003-2004 period. Congress increased the fiscal year 2003 budget request for PAC-3 of 72 missiles by an additional 48 missiles. In late November 2002, DOD approved plans to double PAC-3 monthly production rates, with the number of missiles increasing from four to eight per month after more manufacturing equipment and a second shift of personnel were added. DOD will acquire 108 PAC-3 missiles in FY 2004.
The overall procurement objective of 1,159 PAC-3 missiles remains unchanged. The larger purchases in FY-03 and FY-04 may be offset by lower production in FY-08 and FY-09. Instead of buying 216 missiles in each of those years, DOD would receive 184 units annually.
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David
Fri March 21, 2003 6:49am
|
Patriot PAC-3 ERINT
Patriot Advanced Capability-3 (PAC-3) is a high/medium advanced surface-to-air guided missile air defense system. PAC-3 is a major upgrade to the Patriot system. The PAC-3 Operational Requirements Document (ORD) represents the Army Air Defense need to buy back required battlespace lost against the current and evolving tactical missile and air breathing threat. PAC-3 is needed to ounter/defeat/destroy the 2008 threat and to extend Patriot's capabilities to accomplish new/revised missions. In tandem with the upgraded radar and ground control station, PAC-3 interceptors can protect an area about seven times greater than the original Patriot system.
The PAC-3 Program consists of two interrelated acquisition programs - The PAC-3 Growth Program and the PAC-3 Missile Program. The Growth program consists of integrated, complementary improvements that will be implemented by a series of phased, incrementally fielded material changes. The PAC-3 Missile program is a key component of the overall improvements of the Patriot system, it will provide essential increases in battlespace, accuracy, and kill potential.
PAC-3 is a much more capable derivative of the PAC-2/GEM system in terms of both coverage and lethality. The PAC-3 has a new interceptor missile with a different kill mechanism--rather than having an exploding warhead, it is a hit-to-kill system. The PAC-3 missile is a smaller and highly efficient missile. The canister is approximately the same size as a PAC-2 canister but contains four missiles and tubes instead of a single round. Selected Patriot launching stations will be modified to accept PAC-3 canisters.
The Battalion Tactical Operations Center (BTOC) is an M900 series 5-ton expandable van that has been modified by the addition of data processing and display equipment, and utilized by the battalion staff to command and control the Patriot battalion. The BTOC allows the staff to perform automated tactical planning, communications link planning, and to display situational awareness information.
In the 1997 budget DOD added about $230 million for the PAC-3 through the Future Years Defense Program (FYDP) and established a realistic schedule to lower the program execution risk by extending the engineering and manufacturing development (EMD) phase of the program by ten months. System performance will be improved by re-phasing the missile and radar procurements; upgrading three launchers per battery with Enhanced Launcher Electronics Systems; and extending the battery's remote launch capability. PAC-3 Low-Rate Initial Production (LRIP) will begin in the second quarter of fiscal year 1998, and the First Unit Equipped (FUE) date is planned for the fourth quarter of fiscal year 1999. The FUE capability will consist of 16 missiles and five radars which will be placed in one battalion. As of 1996, in addition to funds being programmed for the Ballistic Missile Defense Organization, the Army planned to spend $9.6 billion for all planned purchases of Patriot missiles, $490 million for modifications and $335 million for product improvements.
The Patriot Advanced Capability 3 (PAC-3) Initial Operational Test and Evaluation (IOTE) began in 2002. The two major objectives of the Initial Operational Test and Evaluation (IOTE) are: (1) To assess the improvements in system performance provided by modifications in terms of operational effectiveness, suitability, and survivability; (2) to verify that modifications do not degrade the existing capabilities. The Initial Operational Test and Evaluation (IOTE) will be the first operational integration and assessment of the complete Patriot Advanced Capability 3 (PAC-3) Configuration 3 system.
The 2nd Battalion 43rd Air Defense Artillery/108th Air Defense Artillery Brigade serves as the test unit for the Initial Operational Test and Evaluation (IOTE). The unit is equipped with the complete package of Patriot Advanced Capability 3 (PAC-3) Configuration 3 hardware, PDB-5+ software and the Patriot Advanced Capability 3 (PAC-3) missile. The Patriot Project Office has issued the upgraded equipment to 2-43 Air Defense Artillery. 2-43 has completed New Equipment Training (NET) and supports testing necessary to obtain material release of the Patriot Advanced Capability 3 (PAC-3) Missile equipment.
The Initial Operational Test and Evaluation (IOTE) is conducted in four phases: (1) The Sustained Operations Phase is a five-day deployment to McGregor Range using approved tactics and doctrine. 2-43 Air Defense Artillery will defend against live aircraft in accordance with threat test support package in a simulated combat environment; (2) The Interoperability Phase is a six-day demonstration of the Patriot Advanced Capability 3 (PAC-3) interoperability with current Army and Joint Theater Missile Defense Systems. This phase is conducted using the Joint Common Simulated Missile Defense System Exerciser or actual tactical equipment; (3) The Flight Mission Simulator (FMS) Phase is a 22-day test of simulated air battles. The mobile Flight Mission Simulator (FMS) is a Patriot missile system simulation used to stimulate and evaluate radar performance, engagement decision and weapon assignment (EDWA) processing and test the Patriot Advanced Capability 3 (PAC-3)’s capabilities against a full spectrum of threat targets; (4) The Missile Flight Test Phase consists of four live missile tests conducted at White Sands Missile Range and Kwajalein Missile Range.
The Air Defense Artillery Directorate of the Operational Test Command conducts the planning and execution of the Initial Operational Test and Evaluation (IOTE). Once Initial Operational Test and Evaluation (IOTE) is complete, the Army Evaluation Center prepares the system evaluation report. This report provides input for the Patriot Advanced Capability 3 (PAC-3) missile Milestone III decision (full rate production) and the materiel release for the complete Patriot Advanced Capability 3 (PAC-3) system.
Four PAC-3 operational tests [some involving more than one interceptor launch] between February 2002 and May 2002 resulted in three launch failures, two misses and one hit that failed to destroy the incoming warhead. A malfunctioning radar and software problems led to the misses, and the launch failures resulted from electrical problems.
The Army received the first 16 PAC-3s -- a full launcher load -- in September 2001. The Army is authorized to produce the missiles at a rate of 72 a year, and Congress authorize an increase to 96 per year in fiscal 2003. The plan is to eventually produce 144 a year, leading to a total inventory of 1,159 interceptors. Unable to certify that the PAC-3 interceptor was ready for stepped-up production, in mid-2002 Pentagon put off the decision for at least a year, and planned on further testing once fixes are in place.
By early 2000 the cost of each PAC-3 missile had increased from $1.9 million to over $4 million, and the estimated total program cost had risen from $3.9 billion to $6.9 billion. After design and manufacturing modifications were initiated to control costs, the estimted cost per missile dropped to about $3 million, and as of mid-2002 program officials expected to reduce the unit cost to $2 million.
Initial reports of a successful intercept of a Patriot missile-as-target by a Pac-3 missile on 25 April 2002 have sinced proven to be incorrect. A US Army statement said that subsequent analysis showed that the Pac-3 impacted the target missile but failed to destroy the warhead, so the intercept was unsuccessful. A second Pac-3 in the same test failed to launch. A PAC-3 missile successfully intercepted a target ballistic missile over Kwajalein Atoll on 30 May 2002. A second missile, however, failed to launch for unknown reasons. A failure to launch also occurred in the last test on 25 April. The target was a modified Minuteman missile with a separating reentry vehicle. This was the last test in the Initial Operational Test and Evaluation (IOT&E) program, prior to a Pentagon assessment of PAC-3’s readiness for full-rate production.
As of late October 2002 the Army had taken delivery of 38 PAC-3 missiles, with another 15 due for delivery by December. The military is under contract to receive an additional 126 missiles over the 2003-2004 period. Congress increased the fiscal year 2003 budget request for PAC-3 of 72 missiles by an additional 48 missiles. In late November 2002, DOD approved plans to double PAC-3 monthly production rates, with the number of missiles increasing from four to eight per month after more manufacturing equipment and a second shift of personnel were added. DOD will acquire 108 PAC-3 missiles in FY 2004.
The overall procurement objective of 1,159 PAC-3 missiles remains unchanged. The larger purchases in FY-03 and FY-04 may be offset by lower production in FY-08 and FY-09. Instead of buying 216 missiles in each of those years, DOD would receive 184 units annually.
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Marissa
Tue March 25, 2003 6:43pm
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An F-16 Fighting Falcon p
An F-16 Fighting Falcon pilot assigned to the 410 Air Expeditionary Wing at a forward deployed location, goes over mission documentation before flight, March 21, 2003. 410 AEW aircraft prepare for take-off for critical sorties on "A-Day" of Operation Iraqi Freedom. Operation Iraqi Freedom is the multinational coalition effort to liberate the Iraqi people, eliminate Iraq's weapons of mass destruction and end the regime of Saddam Hussein.
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David
Fri April 18, 2003 11:33am
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An Iraqi man searches thr
Friday, April 11, 2003, An Iraqi man searches through documents April 11 in Baghdad's military intelligence headquarters for signs of missing relatives who had been seized by the regime before the war.
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Unregistered
Mon July 7, 2003 4:42pm
Rating: 10
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Frisco did such a wonderf
Frisco did such a wonderful job documenting his Vietnam trip.
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