Showing posts with label U.S Air force. Show all posts
Showing posts with label U.S Air force. Show all posts

Thursday, December 29, 2011

RAH-66 Comanche Helicopter Stealthy

The RAH-66 Comanche Comanche is a twin-engine,two-pilot, stealthy armed reconnaissance/attack helicopter. The RAH-66 Comanche intends to feature low observable composite technologies with retractable landing gear and weapons pylon to achieve a low radar cross-section(R CS) and a unique engine exhaust system to suppress its infrared signature. A five-bladed main rotor and a shrouded tail rotor minimize the acoustic and radar signatures.A fly-by-wire flight control system and fully integrated digital avionics assist in piloting the aircraft. The Mission Equipment Package integrates the radar,a forward-looking infrared sensor and an image-intensified television sensor for night flying and target acquisition. The Comanche armament systems are to consist of the Joint Missile/Hellfire Missile, 2.7S-inch aerial rockets,a turreted 2Omm gun, and an air-to-air missile.


The Army intends for RAH-66 Comanche to be a key enabler in achieving the air-ground synergy required for the Army's Future Force. As a component of a Future Force air-ground task force, Comanche units will conduct reconnaissance mobile strike, close combat with ground forces,and vertical maneuver. Comanche's primary role in these operations is to collect and share intelligence information and destroy enemy forces.

The Army received OSD approval for a sixth program restructuring in order to reduce risk and accommodate emerging Future Force requirements in October2 002. The new schedule will add 30 months to Engineering Manufacturing  and Development (EMD), establish a blocked acquisition strategy, and reduce the amount of concurrent developmental testing, 'training, and operational testing. The schedule includes a low-rate initial production (LRIP) decision in FY07, delivery of an initial operational capability in FY09, and a full-rate production decision in FY I O.


The RAH-66 Comanche program is a covered system for LFT &E. The latest revision date for the OSD approved LFT &E Strategy is June 2003. This strategy is an integral part of the updated Test and Evaluation Master Plan. The LFT &E Strategy presents a sequential test program.progressing from components to subsystems and. ultimately. to full-up system-level testing. The full-up system-level test article will be a Block I production representative aircraft. In addition. the strategy includes the lethality testing for the new XMI031 2Omm ammunition being developed for the RAH-66 
Comanche.


RAH-66 Comanche program actions during FYO3 necessary to implement the restructure include the reorganization of the government-contractor development team and the completion of the system-level critical design review. Major assembly of the first EMD aircraft began in August 2003.

In November 2001, Army officials said they were planning on a heavy variant of the RAH-66 as a replacement for the AH-64D. As part of Army transformation plan, Maj. Gen. John Curran, commander of the Army’s aviation center, said that the Comanche could perform the attack as well as the armed reconnaissance mission in the future. It is unclear whether the RAH-66 could maintain its stealthy profile while carrying external weapons, however, and some questions whether Comanche which currently suffers from weight problems has the power and fuel capacity to take on even more weight.

Following a GAO report critical of the Comanche Program14, the Army proposed in late 2001 to restructure the RAH-66 program. The purpose of the restructuring is reportedly to reduce risk by eliminating some of the “concurrency” that currently exists in the program, as well as to address creeping cost growth and schedule slippage. The Army plan is to reduce the number of helicopters built during the program’s EMD phase. The money that is freed up by this strategy would then be used to conduct additional R&D efforts, especially in software development. The Army claims that by reducing risk now, and increasing production later, the Service could save more than $3 billion.

Observers comment that decreasing the number of RAH-66 EMD aircraft could increase the development price $1.5 to $2 billion and add two years to the schedule, fielding an operational version of the Comanche in 2008 (and potentially 2010) rather than the previously scheduled IOC of 2006.16 In late December 2001 it was reported that top DoD acquisition officials, who must approve the Army’s restructuring plan, were still conducting their review.

History Series USAF Aircraft War Vietnam

A-7D Corsair II Fighter
The A-7 was a very capable attack aircraft, bought by both USN and USAF. The design used F-8 Crusader experience in a smaller, subsonic airframe. It was phased out of service recently, but efforts to sell upgraded versions continue. 1551 were built. Began service with Navy, deployed in Southeast Asia by the Air Force in the late summer of 1972, and used in the closing months of the war for tactical bombing and as an escort on gunship missions.



A-1 Skyraider Fighter 
Propeller-driven Navy attack bomber, adapted for use by Air Force. Air Commandos flew the A-1E “Spad” two-seat version. The singleseat A-1H “Sandy” flew escort for rescue operations.



Cessna A-37 Dragonfly Fighter   

Armed variant of the T-37 jet trainer, it was flown by USAF and the South Vietnamese Air Force. It was an effective performer, both in the attack role and as a forward air control aircraft.

 

F-4 Phantom Fighter
Best fighter of the Vietnam War and most versatile. Used for air superiority, dropping bombs, reconnaissance, and forward air control. Originally developed by the Navy, adopted by the Air Force and deployed to Southeast Asia in 1965. Early versions relied on missiles in combat, having no guns. The F-4E had a 20 mm cannon. F-4s accounted for 107 of the 137 MiGs shot down by the Air Force.



F-100 Super Sabre Fighter
USAF’s first supersonic fighter. Used extensively on missions over North Vietnam in the early part of the war. F-100F had two cockpits, was flown by the “Misty” forward air controllers.



F-105 Thunderchief 

The Lead Sled, The Thud. Signature airplane of the Rolling Thunder campaign from 1965 to 1968. Thuds flew 75 percent of the strikes and took more of the losses over North Vietnam than any other type of airplane. F-105Fs flew as Wild Weasel aircraft, finding and destroying surface-to-air missile (SAM) sites.

F-4 Phantom II and F-4E Phantom II US Air National Guard

The big F-4 fighter-bomber was gradually evolved from the F3H, with which it had no more than a configurational similarity. Despite its size and bulky look, the F-4 had excellent performance and good manoeuvrability; it was adopted by both the USN and the USAF. Early F-4’s had no fixed gun, but this was corrected after combat experience in Vietnam showed the need for one. Over 5000 were built, making the F-4 one of the most numerous modern combat aircraft. Many are still in service. Now and then, plans are announced to upgrade the F-4 with new engines and electronics. The RF-4 is a recce version of the F-4 fighter with a camera nose. Currently retired F-4s are being converted into QF-4 target drones.


The 28th May 2008 is the anniversary of the F-4 Phantom II’s maiden. Fifty years ago on 27 May 1958 Bob C. Little had the great honour to lift off in the prototype of probably the most well known fighter aircraft in the western world, the XF4H-1 into the skies over St Louis, Missouri. Actually intended as an interceptor for the US Navy, the new aircraft’s good in flight performance soon made headlines so that a short time later in 1961, the USAF ordered a comparison fly off, code named “Operation Highspeed” against operational counterparts of the day such as the F-104 Starfighter, F-105 Thunderchief und F-106 Delta Dart.



The performance it achieved was so overwhelming that the Phantom, at this time still designated F-110A, left its opponents far behind. In March 1962 the USAF signed initial contracts to procure the Phantom. Only two months later all three Arms of the US Forces changed to a common nomenclature for aircraft types. The F4H-1 became the F-4B and the F-110A was renamed F-4C. The later had minor technical differences in comparison with the “B” version to comply with the requirements of the US Air Force. These included the modified radar unit AN/APQ-100 with improved air-to-ground ability, improved avionics, joy-stick and throttle in the rear cockpit for the WSO. Wider tyres required a deeper wing profile giving an increase in all-up-mass allowing the use of circular under-wing pylons which were to become a characteristic of all later versions of the USAF F-4’s. After the first regular USAF units were deployed to south-east Asia in 1964 the F-4C received its baptism of fire.

The first loss off an F-4 happened on 9 June 1965 as 64-0685 of the 45th TFS ran out of fuel after a air-to-ground mission and the crew had to abandon the aircraft. At the end of the ‘70s’ after USAF Units received the advanced Phantom F-4D and F-4E variants, many F-4C’s were allocated to Squadrons of the US Air National Guard (USANG), where they saw service well into the ‘90s’. Altogether 583 F-4C’s were produced. Even though the F-4C at first sight appears identical to the F-4D, the successor to the ‚C’ model is an autonomous aircraft.



The F-4D Fighter was in reality the version which the USAF wanted in their inventory after the trial flights of 1961 but the requisite technical components were at that time not ready for action. The F-4D had a completely new avionics fit, a new for air-to-ground optimised AN/APQ-109A radar unit, more powerful engines, an improved radar warning suite, a completely re-designed cockpit and the ability to carry LGB’s (Laser Guided Bombs) and other modern Stand-off weapons. Delivery of the first of a total 825 F-4D to operational Units followed in March 1966. One by one it replaced the F-4C on the Front in Vietnam from the spring of 1967 onwards. As more modern aircraft such as the F-15 and the F-16 became available to the US Air Forces in large numbers the remaining F-4D were distributed amongst units of the USANG. As well as the USA, South Korea and Iran also received some models of this variant of the F-4 Phantom II.

Sunday, November 20, 2011

MH-60M Black-hawk and MH-60 SOF Helicopter

Complimenting the MH-47G is the medium lift MH-60M Black-hawk. The SOF Blackhawk comes in two configurations: a troop  transport configuration and a Defensive Armed Penetrator (DAP)  armed configuration. The DAP aircraft provides armed security for  the MH-47G and other MH-60 aircraft. The MH-60M modernization  program will begin delivering new-build MH-60M aircraft this year.  Once complete, the MH-60M modernization program will provide  the 160th SOAR with 70 MH-60M SOF-unique Blackhawks.
MH-60M Black-hawk

The MH-60 SOF modernization program takes Sikorsky’s new build UH-60M aircraft from the U.S. Army and modifies them with SOF-unique mission equipment. The MH-60M aircraft will feature CAAS, SIRFC, wide-chord rotor blades, active vibration reduction,  and the improved Electro-Optical Sensor System. The most sig- nificant modification, however, is the incorporation of two General Electric YT706-GE-700 engines. These 2,500 shaft horsepower engines give the aircraft a high/hot capability unmatched by any
H-60 variant currently fielded. As the MH-60M is fielded, 160th SOAR will continue phasing out the current MH-60K/L fleet.

Friday, September 23, 2011

A-4 SkyHawk Small Fighter

This A-4 SkyHawk is small and simple tailed delta jet, originally designed as carrier-based (nuclear) bomber, later enjoyed a long career as an extremely versatile attack aircraft. Later developments had a large dorsal spine to make room for electronics. The A-4 was kept in production for 22 years, and is still serving with some air forces. The OA-4 is a two-seat FAC version for the USMC, and the trainer version is known as TA-4. 2960 built.

A-4 SkyHawk
A-4 SkyHawk Fighter
A-4 SkyHawk Aircraft
A-4 SkyHawk
A-4 SkyHawk Specifications

Type A-4F A-4M
Function attack attack
Year 1966 1966
Crew 1 1
Engines 1 * 41.4 kN P&W J52-P-8A 1 * 5080 kg P&W J52-P-408A
Wing Span 8.38 m 8.38 m
Length 12.22 m 12.29m
Height 4.57 m 4.57 m
Empty Weight 4536 kg 4747 kg
Max.Weight 11113 kg 11113 kg
Speed 1100 km/h 1078 km/h
Ceiling 14940 m 12880 m
Armament 2*g20mm, 3720kg 2*g20 mm 4153 kg

A-5 Vigilante and RA-5C Vigilante Fighter Nuclear Bomber

The A-5 Vigilante fighter was a very advanced supersonic attack aircraft, optimized for low-level attacks at high speed. It was long and angular, with rectangular air intakes, small, thin swept wings incorporating large full-span flaps, and all-moving tail surfaces. But the A-5, one of the biggest aircraft ever operated from a carrier, was not successful in its intended role as nuclear bomber, It has been claimed that the bomb ejection mechanism was unsatisfactory. The bomb bay was between the engines, and the plan was to expell the bomb rearwards, together with two empty fuel tanks. 63 bombers were built, but all but ten were converted to RA-5C reconnaissance aircraft. There were also 55 new RA-5Cs built. These were very effective and served until 1980.

A-5 Vigilante Fighter
A-5 Vigilante History

Designed to meet a US Navy requirement for a high-performance all-weather attack aircraft, the North American NA-247, known at first as the NAG-PAW (North American General Purpose AttackWeapon), won an order for two YA3J-1 prototyes on 29 June 1956. The name Vigilante was allocated soon after this, and teh A3J designation was changed subsequently to A-5. The design’s cantilever monoplane swept wing incorporated no ailerons, roll control being by the use of spoilers in conjunction with differential use of an all moving tailplane on each side of the fuselage and, when it entered service, the Vigilante was the first US production aircraft to introduce variable geometry intakes for its two General Electric J79 engines.

RA-5C Vigilante Fighter
The first of the prototypes, then powered by two YJ79-GE-2 engines each developing 6804-kg (15,000lbs) afterburning thrust, was fown for the first time on 31 August 1958, and carrier trials were completed abourd the USS Saratoga in July 1960. Initial productino version A-5A, US Navy Squadron VAH-7 becoming the first operational unit in June 1961. The primary weapon of the A-5A was a free-fall nuclear bomb ejected rearwards from a bomb bay between the tailpipes of he two turbojet engines. A-5A prduction totalled 57
aircraft. This version was followed by an interim long-range bomber version designated A-5B, incorporating greater fuel capacity and aerodynamic improvements, but, because of changes in the US Navy policy only six were built and then converted to serve as a long-ranged unarmed reconaissance verson designated RA-5C, equipped with side-looking airborne radar, cameras and electronic counter-measures equipment.

A5 Vigilante Aircraft
RA-5C Vigilante Fighter


The first RA-5C Vigilante Fighter flew on 30 June 1962, being followed by 55 new production aircraft and the conversion to reconnaissance configuration of the 53 A-5As. The first squadron equipped with the RA-5C was RVAH-5 which, in June 1964, was operating fromt he USS Ranger, and other Vigilante squadrons included RVAH-1, RVAH-7, RVAH-9, and RVAH-11.

Specifications
RA-5C Vigilante:
Type: carrier-based long-range reconnaissance aircraft
Powerplant: 2 8101-kg(17,860lb) afterburning thrust General Electric J79-GE-10 turboets

Performance:
max speed-Mach 2.1
operational ceiling-14,750 m (48,400 ft)
range-4828 km (3,000 miles)

Weights:
empty-17009 kg (37498 lbs)
max take-off weight-29937 kg (66,000 lbs)

Dimensions:
span-16.15m (53ft)
length-23.32m (76.5ft)
height-5.91m (19 feet 4.75 inches)
wing area-70.05m2 (754 sq ft)

Friday, June 10, 2011

HH-60G Pave Hawk Helicopter In Target Mission

HH-60G Pave Hawk Mission :

Conduct day/night/marginal weather alert response missions to recover downed aircrew or other isolated personnel in hostile or permissive environments; perform disaster relief, noncombatant evacuation operations,
counter-drug operations, civil search and rescue, and Space Shuttle support.

Description :

The HH-60G Pave Hawk provides Combat Search and Rescue (CSAR) and Personnel Recovery (PR). It is the most rapidly deployable, long range, combat rescue helicopter in the Air Force inventory. The Pave Hawk is a highly modified version of the Army Black Hawk helicopter. It features an upgraded communications and navigation suite that includes integrated inertial navigation/global positioning/Doppler navigation systems, satellite communications, secure voice, and Have Quick communications.

All HH-60Gs have an automatic flight control system, night vision goggles lighting, and forward looking infrared system that greatly enhances night low-level operations. The Pave Hawk has color weather radar and an engine/rotor blade anti-ice system that gives the HH-60G adverse weather capability. Pave Hawk mission equipment includes a retractable in-flight refueling probe, internal auxiliary fuel tanks, and two crew-served 7.62mm/.50cal machine guns.

Pave Hawk combat enhancements include a radar warning receiver, infrared jammer, and a flare/chaff countermeasure dispensing system. HH-60G rescue equipment includes a hoist capable of lifting a 600-lb. load (270 kilograms) from a hover height of 200 feet (60.7 meters), and a personnel locating system that is compatible with the PRC-112 survival radio. It provides range and bearing information to a survivor’s location. A limited number of Pave Hawks are equipped with an over-the-horizon tactical data receiver that is capable of receiving near real-time mission update information.

  
Program Status

Weight : 22,000 lb.

- Range : 500 nautical miles (NM)

- Armament : M-240 7.62 machine gun, GAU-2C-7.62mm mini-gun, GAU-18 .50 caliber machine gun

- Dimensions Main Rotor: 53 ft.; Length: 64 ft.; Height: 16 ft.

- Service Ceiling : 14,200 ft.

- Self-Protection : Integrated Chaff/Flare/RWR, Infra-red (IR) Jammer, Kevlar armor, Self-sealing fuel tanks

- Speed : 125 knots

- Other Specifications : Communications UHF Line-of-Sight (LOS), VHF LOS, Secure UHF Satellite Communications (SATCOM)/DAMA, Personal Locator System (PLS), HQ-II; Navigations: Integrated INS/ GPS/Doppler Forward Looking Infrared (FLIR), over-thehorizon
(OTH) Tactical Receiver, Digital Moving Map/Threat Display, WX Radar, and Hoist

F16-TARS Theater Airborne Reconnaissance System

F16-TARS (Theater Airborne Reconnaissance System) Mission

Provide warfighting theaters with organic, survivable, and responsive penetrating tactical reconnaissance that gathers timely, high-quality imagery intelligence data for use by commanders in the air-land battle.


F16-TARS



 Description

The F16-TARS (Theater Airborne Reconnaissance System) consists of a removable pod uploaded to F-16C Block 25/30/32 aircraft. TARS is the Air Force’s only high-speed, penetrating, under-the-weather, theater-controlled, reconnaissance capability. In the span of a single engagement, it provides unique rapid strike and reconnaissance in a high-threat environment. Per the 2004 operational requirements document and
as requested by CENTAF, TARS must provide near-real-time imagery transmission to forces on the ground, allowing immediate response to threats and battle damage assessment (BDA).



F16-TARS


 Continuously deployed in Iraq since May 2005, TARS has significantly increased imagery available in Operation Iraqi Freedom (OIF) by producing over 6,000 images for CENTCOM in support of infantry and special operations personnel engaged in counter insurgent pre-raid planning, time-sensitive targeting, BDA, and counter-IED support. Data link capability will begin limited fielding in FY07

Specifications






 Acquisition Status 

Program Status :   Sustainment
Future Upgrades : Datalink for near-real-time data transmission

MH-53 Pavelow Helicopter Series III and IV

MH-53 Pavelow  Mission

Provide low-level, long-range, undetected penetration into denied areas day or night, in adverse weather for infiltration, exfiltration, and resupply of special operations forces.

Descreption :

MH-53J/M Pave Low III/IV missions are almost always conducted under cover of darkness and frequently under adverse weather conditions requiring extended flight operations as low as 50 feet using night vision goggles or Instrument Meteorological Conditions as low as 100 feet above ground level. Missions involve deep penetrations of hostile areas at extreme ranges without escort. The MH-53J/M employs a sophisticated avionics system to enhance crew situational awareness and avoid threats.


Specifications :

Weight : 46,000 lb. (gross weight)

Range: 600 nautical miles (NM); unlimited with helicopter air refueling

Armament: Two 7.62 mm Mini-Guns; one .50 Caliber Machine Gun

Dimensions Length: 88 ft.; Height: 25 ft.; Roto Diameter: 72 ft.


Acquisition Status

Program status : Modifications only

Manucakture 

Airframe - Sikorsky (CT); Engine/Gear Box - Lockheed Martin (GA); Radar/Forward Looking Infrared (FLIR) - Raytheon (TX); General Mods - EJM (FL); MTC (GA).

MH-53 Pave Low Helicopter Video

F-16 HARM Targeting System (HTS) R6 and R7

F-16 HARM Targeting System (HTS) R6 and R7 Mission

Descreption

The F-16 High-Speed Anti-Radiation Missile (HARM) targeting system detects and provides targeting information on enemy air defense radar outside the lethal range of their associated surface-to-air missiles (SAM). The system supports the F-16’s Suppression/Destruction of Enemy Air Defenses (SEAD/DEAD) mission. The HARM Targeting System (HTS) enables employment of the AGM-88 HARM in the “range known” mode the missile’s most lethal mode.

F-16 HARM

HTS targeting information increases HARM lethal range by 25 percent and increases the probability of hitting the target radar. The HTS Release 7 version will provide a precision targeting capability needed for accurate employment of GPS-aided munitions as well as HARM, with increased situational awareness and detection range.

Specification 


Fighter F-16 Fighting Falcon Aircraft Next Generation

Fighter F-16 Fighting Falcon Mission Target

Provide low-cost, high-performance, air-to-air combat and air-to-surface attack capability.

F-16 Fighting Falcon


Descreption

The F-16 Fighting Falcon is a compact, maneuverable, multi-role fighter aircraft that is proven in air-to-air combat and air-to-surface attack. The F-16’s maneuverability and combat radius (distance it can fly to enter air combat, stay, fight and return) exceed that of potential threat fighter aircraft. It can locate targets in all weather conditions and detect low flying aircraft in radar ground clutter. In an air-to-surface role, the F-16 can fly more than 500 miles (860 km), deliver its weapons with superior accuracy, defend itself against enemy aircraft, and return to its starting point.

F-16 Fighting Falcon

In designing the F-16, advanced aerospace science and proven reliable systems from other aircraft such as the F-15 and F-111 were selected and combined to simplify the airplane and reduce its size, purchase price, maintenance costs and weight. Fully fueled, the F-16 can withstand up to nine G’s—nine times the force of gravity. Avionics systems include a highly accurate inertial navigation system coupled with a GPS by which a computer provides steering information to the pilot.

F-16 Fighting Falcon

The plane has UHF and VHF radios, instrument landing system, a warning system, and modular countermeasure pods to be used against airborne or surface electronic threats. During Operation Iraqi Freedom (OIF) the F-16 continued its superior performance in precision strike missions using a variety of GPS and laser guided weapons. Currently, the F-16 comprises 53 percent of the Air Force fighter force structure and provides 67 percent of the precision guided munitions capability in our Air Expeditionary Forces.

Specifications 











Acquisition Status










Contractors
Prime : Airframe - Lockheed Martin (TX); Engines - Pratt & Whitney (CT); General Electric (OH)

Subcontractors : Northrop Grumman (MD); Raytheon (TX); Israel Aircraft Industries (Israel); Honeywell International (CA, NJ, NM, MN)

AGM-86B Air Launched Cruise Missile (ALCM)

AGM-86B Air Launched Cruise Missile (ALCM) Mission

Provide a highly accurate, long-range, air-to-surface strategic nuclear missile that can evade air and ground-based defenses to strike targets anywhere in the enemy’s territory.

AGM-86B Missile

Description :
The AGM-86B Air Launched Cruise Missile (ALCM) is a highly accurate, long-range, air-to-surface strategic nuclear missile. It carries a single W80 nuclear warhead. The small, winged AGM-86B missile is powered by a turbofan jet engine that propels it at sustained subsonic speeds. After launch, the missile’s folded wings, tail surfaces, and engine inlet deploy.


 The AGM-86B is then able to fly complicated routes to a target through use of a terrain contour-matching guidance system. AGM-86B missiles can be air-launched in large numbers by B-52 bombers. An enemy force would have to counterattack each of the missiles, making defense against them costly and complicated.
The missiles’ small size and low-altitude flight capability make them difficult to detect on radar.

AGM-86B Missile on Bomber


Spectifications :

Weight : 3,150 lb.

Range : 1,500+ miles

Armament : W80-1 warhead

Dimensions Length : 20.75 ft.; Diameter: 2 ft.; Wingspan: 12 ft.

Warhead W80-1 warhead

Coverage : Global

Compatability : B-52

Acquisition status

Program Status : Fielded
Unit Assignment :
Barksdale AFB, LA; Minot AFB, ND
Future Upgrades :
Undergoing life extension programs

E-3 Sentry Airborne Warning and Control System (AWACS)

E-3 Sentry Warning and Control System (AWACS) Target Mission

Provide all-weather surveillance, command, control, and communications needed by commanders of U.S., NATO, and other allied air defense forces.

E-3 Sentry Airborne



Description
The E-3 Sentry Airborne Warning and Control System (AWACS) aircraft provides responsive and flexible real-time command and control/battle management in support of worldwide operational employment of U.S. and coalition forces. AWACS provides persistent and survivable surveillance, battle management, weapons control, threat warning, and combat ID information in support of commander taskings.

E-3 Sentry Airborne
It gives commanders a self-contained and worldwide, around-the-clock capability to prosecute air and ground campaigns. The E-3 Sentry is a modified Boeing 707/320 commercial airframe with a rotating radar dome. The radar combined with an identification friend or foe subsystem can look down to detect, identify, and track enemy and friendly low-flying aircraft by eliminating ground clutter returns that confuse other radar systems. Other major subsystems in the E-3 include navigation, communications, computers (data processing), and displays.

Specifications


Size 
 Length: 145 ft., 8 in. (44 m); Wingspan: 130 ft., 10 in.
(39.7 m); Height: 41 ft., 4 in. (12.5 m)

Weight  
347,000 lb. (156,150 kg)

Range  
More than eight hours (unrefueled)

Coverage
The radar has a range of more than 250 miles (375.5 km) for
low-flying targets and farther for aerospace vehicles flying
at medium to high altitudes

 Acquisition Status


Program Status :  The AWACS Block 40/45 Upgrade is in the middle of System Development and Demonstration (SDD). It includes several projects aimed at reducing operator workload, providing a fused air picture to the warfighter, and transmitting that air picture off-board in a more timely manner Integrated.
Demand Assigned Multiple Access (DAMA) Global Air Traffic Management (GATM) (IDG) expands user availability of severely limited DoD UHF SATCOM channels through the use of DAMA and meets mandate for International Civil Aviation compliance on near-term air traffic control navigation requirements. The AWACS fleet is currently being modified with IDG.

Unit Assignment : 552 Air Control Wing, Tinker AFB, OK

Current Inventory : 32 operational aircraft and 1 test aircraft

F-117 Nighthawk Aircraft In War

F-117 Nighthawk Target and Mission


Penetrate high-threat air space, using low-observable stealth technology, and conduct precision strikes against critical, robustly defended targets.



Description

The F-117 Nighthawk is the world’s first operational aircraft designed to exploit low-observable stealth technology and use laser-guided and GPS-guided weapons against critical targets. The unique design of the single-seat F-117 provides exceptional combat capabilities. About the size of an F-15 Eagle, the twin-engine F-117 aircraft is powered by two General Electric F404 turbofan engines and has quadruple redundant fly-by-wire flight controls. Air-refuelable, the F-117 supports worldwide commitments and adds to the deterrent strength of U.S. military forces.



 Specifications











F-35 Lightning II Joint Strike Aicrfat In Target Mission


F-35 Lightning II Joint Strike Fighter Target Mission

Provide all-weather, precision, stealthy, air-to-ground strike capability, including direct attack on the most lethal surface-to-air missiles (SAMs) and air defenses; meet the requirements of the three U.S. Services, the UK, and other allies.
F-35 Lightning


 Description
 
The F-35 Lightning II, Joint Strike Fighter (JSF) program will develop and deploy an affordable, fifth-generation, stealthy, multi-role strike fighter aircraft. The Conventional Takeoff and Landing (CTOL) F-35 will be used to support the Air Force core competencies of Air and Space Superiority, Global Attack, Precision Engagement, and Agile Combat Support. 


F-35 Lightning

The F-35 will complement a force structure that includes fighter, bomber, and support assets operating in an environment with F-22A and within the projected Command, Control, Communications, Computers, Intelligence, Surveillance, and Reconnaissance (C4ISR) architecture. The F-35 capitalizes on system commonality and modularity among variants, maximizing affordability and logistical support for 21st century AEF employment. 

F-35 Lightning II


The service versions of the F-35 include the following:
 
• USAF: F-35A CTOL, stealthy, multi-role aircraft (primary air-to-ground) to replace
the F-16 and A-10 and complement the F-22A
• USMC: F-35B (Short Takeoff and Vertical Landing (STOVL)), stealthy, multi-role strike
fighter to replace the AV-8B and F/A-18
• USN: F-35C (Carrier Version (CV)), stealthy, multi-role strike fighter to complement
the F/A-18E/F
• UK: F-35B STOVL aircraft to replace the Sea Harrier and GR-7

 Specifications















Acquisition Status 

 
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