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Japan space scientists make wireless energy breakthrough



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Japanese scientists have succeeded in transmitting energy wirelessly, a key step that could one day make solar power generation in space a possibility, an official said.

Researchers used microwaves to deliver 1.8 kilowatts — enough to run an electric kettle — through the air with pinpoint accuracy to a receiver 55 meters (170 feet) away.


While it wasn’t a great distance, the technology could pave the way for mankind to eventually tap the vast amount of solar energy available in space and use it here on Earth, a spokesman for The Japan Aerospace Exploration Agency (JAXA) said Thursday.

“This was the first time anyone has managed to send a high output of nearly 2 kilowatts of electric power via microwaves to a small target, using a delicate directivity control device,” he said.

JAXA has been working to devise space solar power systems, or SSPSs, for years, he said. Solar power generation in space offers many advantages, notably the permanent availability of energy regardless of weather or time of day.

While man-made satellites, such as the International Space Station, have long been able to use the solar energy that washes over them from the sun, getting that power down to Earth where people can use it has been a thing of science fiction.

But the Japanese breakthrough offers the possibility that humans will one day be able to tap an inexhaustible source of energy in space.

The idea, said the JAXA official, would be for microwave-transmitting satellites with sunlight-gathering panels and antennae to be set up about 36,000 km (22,300 miles) from Earth.

“But it could take decades before we see practical application of the technology — maybe in the 2040s or later,” he said.

“There are a number of challenges to overcome, such as how to send huge structures into space, how to construct them and how to maintain them,” he said.

The SSPS concept emerged in the U.S. in the 1960s. Japan’s version, mostly financed by the industry ministry, started in 2009, he said.

Resource-poor Japan has to import huge amounts of fossil fuel. It has become substantially more dependent on these imports as its nuclear power industry shut down in the aftermath of the disaster at Fukushima in 2011

Mitsubishi Heavy Industries Ltd. meanwhile said Thursday it succeeded in transmitting 10 kilowatts wirelessly to a receiver 500 meters away, in a test in Kobe. It hopes to find practical applications for the technology in five years, such as for charging electric vehicles or powering warning lights on power transmission towers. The company also said it aims to use the technology to send power to isolated areas in the wake of disasters.

Mitsubishi Heavy has cut costs by using a mechanism employed in microwave ovens because the cost of wireless power transmission technology used in space is high, according to the company. The company plans to eventually halve the cost.

At present, a more efficient system is needed to transmit power from offshore wind turbines and send electricity to isolated rural areas, Mitsubishi Heavy said


Japanese scientists make breakthrough in wireless energy transmission | The Japan Times
 
MCMRON-7 and JMSDF Focus on Combined Operations in Annual Mine Warfare Staff Talks


WHITE BEACH, Okinawa (NNS) -- Commander, Amphibious Force U.S. 7th Fleet, Commander, Mine Countermeasures Squadron (MCMRON) 7, and Japan Maritime Self Defense Force Commander (JMSDF), Mine Warfare Force concluded a three day mine warfare staff conference at CTF 76 headquarters Feb. 25.

This year's conference highlighted an increased focus on enhancing combined exercises to better integrate U.S. and Japanese forces and capabilities in a live-force environment. Interoperability, cooperation, and tactical development were key themes of the event.

"These talks are another example of the exceptional relationship enjoyed by the U.S. Navy and JMSDF, said Rear Adm. Hugh Wetherald, commander, Amphibious Force U.S. 7th Fleet. "The fact that we can come together to discuss openly on how we can improve our core combat capabilities and interoperability in mine warfare and amphibious operations demonstrates our commitment to this alliance."

The intent for the staff talks is to provide a forum for the subject matter experts to meet and discuss different aspects of their mission objectives and their responsibilities and provide a forum to discuss coordination and training between U.S. and JMSDF mine warfare forces.

"Our ability to operate seamlessly with our JMSDF counterparts in such a critical area of the world is vital to maintaining stability and open seas in the Western Pacific" said Capt. Mike Dowling, commander of MCMRON-7. "We genuinely appreciate the professionalism and knowledge of our friends in the JMSDF Mine Warfare Force."

Both U.S. and JMSDF MCM ships pulled into White Beach where Sailors from both navies were provided tours and introductions of the ships as their respective staffs crafted plans for future operations. In the spirit of friendship, the two navies engaged in softball and enjoyed a cookout serving traditional American and Japanese barbeque.

MCMRON-7, commanded by Capt. Mike Dowling, is a combined readiness and tactical staff responsible for mine countermeasures in the U.S. 7th Fleet area of responsibility. The squadron consists of four Avenger-class minesweepers forward deployed to Sasebo, Japan, and a helicopter mine countermeasures detachment in Pohang, Republic of Korea.




MCMRON-7 and JMSDF Focus on Combined Operations in Annual Mine Warfare Staff Talks
 
I do not know what happened to the JMSDF-PN thread so I'll just post photos here. More on PASSEX from jmsdf fb page.
 

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JASDF E-767 AWACS

  • Primary Function Airborne surveillance and command and control
  • Crew 21 mission specialists
  • Flight Crew 2
  • AWACS Officers 19
  • AWACS 767 Aircraft Designation 767-27C
  • Japan Air Self-Defence Force Aircraft Designation E-767
  • Armament None
The Boeing 767 AWACS airborne warning and control system has been selected by Japan to carry out airborne surveillance and command and control (C2) operations for tactical and air defence forces. The surveillance system is based on a flexible, multimode radar, which enables AWACS to separate maritime and airborne targets from ground and sea clutter radar returns.

Production of the 707 airframe, which has been used since 1977 for the E3 AWACS, ended in May 1991. Following studies of the most suitable follow-on aircraft for the AWACS mission, Boeing announced in December 1991 that it would offer a modified Boeing 767 jet as the platform for the system.

Boeing 767 AWACS programme and development
Aircraft No 1 and No 2 were delivered to the company's first customer, the Government of Japan, in March 1998. The final two aircraft were delivered in January 1999. All four aircraft entered service with the Japanese Air Self-Defense Force (JASDF) in May 2000. Boeing delivered the 50th 767 jetliner to Japan Airlines in July 2009. The Boeing 767 is being operated in more than 130 countries worldwide.

All Nippon Airways (ANA) awarded a contract worth $2bn to Boeing in December 2009 for supply of five 777 and five 767 jetliners.

The aircraft is flown by two pilots rather than four aircrew as on the E3 AWACS. There are 18 AWACS mission crew led by a mission director and a tactical director.

Boeing 767 AWACS airframe
"The Boeing 767 AWACS carries out airborne surveillance and command and control (C2) operations for tactical and air defence forces."
The wide-body configuration of the 767 offers 50% more floor space and nearly twice the volume of the 707. The basic 767 airplane is manufactured by Boeing Commercial Airplane Group in Everett, Washington, and then flown to Boeing Information, Space & Defense Systems facilities in Wichita, Kansas, where the airframe is modified to accommodate the prime mission equipment. All aircraft are returned to the Boeing Seattle facility, where mission equipment and the rotodome are installed.

Major subcontractors include Northrop Grumman, General Electric, Rockwell Collins and Telephonics, which have been involved in the previous Boeing AWACS programs.

AWACS radar
The antenna systems for primary radar and the information friend or foe (IFF) interrogator are mounted in a 9.1m diameter circular radome above the aircraft fuselage. The primary radar is the AN/APY-2, developed for E3 AWACS by Northrop Grumman in Baltimore. The radar operates at about 10GHz (wavelength about 10cm) in the E/F bands. It scans mechanically in azimuth at six revolutions per minute, and electronically in elevation. In flight, when the radar is not operational, the slip rings and bearings are kept lubricated by rotating the radome at one cycle every four minutes.

The main modes of operation of the radar are: pulse Doppler non-elevation scan; pulse Doppler elevation scan; beyond-the-horizon mode; maritime mode for detection of surface ships; combined operational modes using data interleaving for long-range detection; and passive mode operation in which the transmitters are switched off for radar-silent operations.

"At operating altitude, AWACS can detect targets over 320km away."
The AWACS radar provides a 360° view of the area. At operating altitudes it can detect targets more than 320km away. Targets are separated and individually managed and displayed on situational displays.

In May 2006, Japan requested the foreign military sale of four radar system improvement programme (RSIP) kits, as fitted on USAF, UK and Nato E-3 AWACS.

Northrop Grumman was awarded the contract for the upgrade in December 2006. The RSIP upgrades the capability against threats from small radar cross section targets, cruise missiles and electronic countermeasures.

The improvement in sensitivity against small and stealthy targets is achieved through a new surveillance radar computer to replace the digital Doppler processor and radar correlator, and the translation of the associated software into ADA language.

AWACS mission equipment
The main AWACS operations cabin behind the flight deck is laid out in equipment bays for communications, data and signal processing, navigation, and identification equipment. The AWACS officers and operator stations are equipped with Hazeltine command and control consoles fitted with high-resolution colour displays. The main signal and data processing computer, Lockheed Martin CC-2E, has a main storage capacity of over three million words; five times larger than that of the CC-2 computers installed on the E3 AWACS aircraft.

The AWACS mission equipment on the 767 AWACS takes advantage of the combat-proven avionics currently employed on-board operational AWACS aircraft, and is interoperable with the AWACS aircraft currently in service.

"The AWACS radar provides a 360° view of the area."
The aircraft's navigation system is based on two LN-100G inertial navigation systems with integrated satellite global positioning systems, supplied by Northrop Grumman (formerly Litton).

Turbofan engines
The 767 aircraft is powered by two General Electric CF6-80C2B6FA turbofan engines, providing 61,500lb thrust. The more powerful engines on the 767 AWACS compared to the 707/E3 AWACS allow the aircraft to carry a heavier payload, have a greater range and to fly higher.

Two electrical generators are fitted on each of the two engines, producing a total of 600kW.

Performance
The 767 AWACS aircraft can fly at a maximum speed of 800km/h. The range and service ceiling of the aircraft are 10,370km and 12,222m respectively. The endurance of the aircraft is 13 hours at 300nm radius. The aircraft weighs 85,595kg, while the maximum take-off weight is 175,000kg.

Boeing 767 AWACS Airborne Warning and Control Aircraft - Airforce Technology

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Japan begins process of E-767 AWACS upgrade

Gareth Jennings, London

28 October 2014

Boeing is to begin the upgrade of Japan's fleet of E-767 Airborne Warning and Control System (AWACS) aircraft with a USD25.6 million design and production contract announced by the US Department of Defense (DoD) on 28 October.

The four aircraft, which have been in service with the Japan Air Self-Defense Force (JASDF) since 1998-99, will each be fitted with new systems, and three ground support facilities will also be upgraded under the programme.

Specifically, the aircraft will be equipped with updated mission computers, electronic support measures, a traffic alert and collision avoidance system, AN/APX-119 interrogator friend or foe (IFF) transponder, next-generation UPX-40 IFF, automatic identification system, and datalink upgrades.

According to the DoD, this modernisation work "will allow Japan's AWACS fleet to be more compatible with the US Air Force [Boeing E-3 Sentry] AWACS fleet baseline, and provide for greater interoperability".

The design and production work will be performed by Boeing in Washington state, and is expected to be completed by 28 February 2015. According to a US Defense and Security Cooperation Agency (DSCA) notification into the upgrade that was released in late 2013, the total value of the programme, including installation, is USD950 million.

This design and production contract follows an initial Mission Computing Upgrade (MCU) contract for the E-767 AWACS fleet that is set to be completed by 31 December 2014.

COMMENT

Japan is the only operator of the E-767 AWACS platform, with the other AWACS users of France, NATO, Saudi Arabia, the United Kingdom, and the United States opting instead to utilise the 707-based E-3 airframe.

Given the existing incompatibility issues with regard to airframe support, the JASDF is keen that the mission hardware and software of its E-767 platforms remain compatible with those of the other AWACS operators in general, and with those of the United States in particular. This contract will begin the upgrade process that will go a long way towards achieving that.

Japan begins process of E-767 AWACS upgrade - IHS Jane's 360

More Details:
Japan Orders Upgrades for its 4 E-767 AWACS
 
JASDF E-2C Hawkeye AWACS

13 Units - First Delivered in 1984. E-2C 2000 Configuration (Please see attached PDF)
4 Units will be purchased this year - E2-D configuration


E-2C Hawkeye 2000

The all-weather E-2 Hawkeye airborne early warning and battle management aircraft has served as the "eyes" of the U.S. Navy fleet for more than 30 years, and the E-2C Hawkeye 2000 possesses the most advanced AEW&BM capabilities in service today. Continuous modifications and upgrades have kept the aircraft's mission systems current with the evolving operational environment. The next generation E-2D Advanced Hawkeye, the key airborne enabler of the US Navy's FORCEnet began test flights in 2007.

Hawkeye 2000
Hawkeye 2000 is the fifth generation production E-2C Hawkeye and incorporates significant enhancements in data management, system throughput, operator interfaces, connectivity, and situational awareness to support the Navy's evolving Theater Air and Missile Defense mission. This Hawkeye capitalizes on the previous version Group II baseline fully integrated system, which includes the AN/APS-145 radar system, improved identification friend/foe (IFF) system, the Joint Tactical Information Distribution System (JTIDS), a global positioning system (GPS) and the Carrier Aircraft Inertial Navigational System (CAINS) II navigation system.

At the core of the Hawkeye 2000 system's configuration is the open architecture central mission computer. The computer capitalizes on commercial off-the-shelf (COTS) technology, to provide the memory, processing power, and data throughput to support the Hawkeye mission system's growth. The computer capability is accompanied by COTS technology tactical workstations, referred to as the Advanced Control Indicator Set (ACIS), which provides each operator with greater flexibility in display management and presentation.


Integrated into the Hawkeye 2000 and key to the Theater Air and Missile Defense mission is the Cooperative Engagement Capability (CEC) system. This new system provides a high capacity data exchange of detailed target information to the carrier's command center and surface combatants for enhanced fleet-wide connectivity and situational awareness. The cooperative engagement processor facilitates the network's data exchange with onboard tactical information and enables relay to extend surface long-range connectivity.

The Hawkeye's vast communications suite has been expanded with a fully integrated satellite communications (SATCOM) capability. Incorporation of a SATCOM radio communications set and the Multimission Advanced Tactical Terminal (MATT) provides the Hawkeye with an expanded over-the-horizon (OTH) wide-band and narrow-band voice and data communications capability for enhanced situational awareness of the Hawkeye's surveillance volume and beyond.

An electronic support measures (ESM) system upgrade provides enhanced electronic emissions detection, identification, and monitoring capabilities utilizing fewer system components that significantly reduces weight and volume.

The growth of the avionics system's cooling requirements has been addressed through incorporation of a higher capacity cooling system. This system utilizes an environmentally friendly refrigerant.

The aircraft also incorporates several producibility, reliability, and maintainability improvements, modular main power distribution box, a redesigned fault reporting system, and numerous other aircraft improvements.
E-2C Hawkeye 2000


E-2C Hawkeye radome and mission systems

The large 24ft diameter circular antenna radome above the rear fuselage gives the E-2C its distinctive profile. The radome houses the AN/APA-171 antenna supplied by Randtron Systems, which rotates at 5rpm to 6rpm.

The Lockheed Martin AN/APS-145 radar is capable of tracking more than 2,000 targets and controlling the interception of 40 hostile targets. One radar sweep covers six million cubic miles. The radar's total radiation aperture control antenna reduces sidelobes and is robust against electronic countermeasures. It is capable of detecting aircraft at ranges greater than 550km. The Lockheed Martin AN / UYQ-70 advanced display system and computer peripherals provide operators with multicolour displays, map overlays, zoom facilities and auxiliary data displays.

In August 2005, Northrop Grumman completed the E-2C mission computer replacement programme, with the provision of faster, more powerful and reliable computers.
E-2C/D Hawkeye Early Warning Aircraft - Airforce Technology


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JASDF F-2 Fighter

Key Data

  • Wingspan 10.8m
  • Span of Tailplane 6.05m
  • Length 15.52m
  • Height 4.96m
  • Empty Weight 12,000kg
  • Internal Fuel Capacity 3,600kg
  • Maximum Speed Mach 2
The F-2 support fighter aircraft is a multi role single engine fighter aircraft principally designed for the Japan Air Self Defence Force (JASDF), the result of a joint Japan and USA development programme. Mitsubishi Heavy Industries (MHI) is the prime contractor and Lockheed Martin Aeronautics Company serves as the principal US subcontractor. The F-2A is the single-seat version and F-2B is the two-seat version.

The Japanese Defence Agency originally planned to procure a total of 130 F-2 aircraft (83 single-seat and 47 two-seat aircraft) with deliveries to beyond 2010, but, in early 2007, this number was reduced to 94.

"The F-2 fighter aircraft can also carry 500lb bombs, CBU-87/B cluster bombs and rocket launchers."
The initial order was for 81 aircraft. A further five were ordered in March 2007 in a $150m contract. MHI awarded a further $250m contract to Lockheed Martin in April 2008 to manufacture components for eight more F-2 aircraft. The contract was the 12th annual contract awarded by MHI to Lockheed Martin.

F-2 fighter programme and development
In 1987, the JASDF selected a variant of the F-16C as the Japanese FS-X aircraft to replace the Mitsubishi F-1 aircraft, and in 1988 Mitsubishi was selected as prime contractor for the aircraft, which became known as the F-2. The programme involved technology transfer from the USA to Japan, and responsibility for cost sharing was split 60% by Japan and 40% by USA.

Four flying prototypes were developed, along with two static prototypes for static testing and for fatigue tests. Flight trials of the prototypes were successfully completed by 1997, and the aircraft entered production in 1998.

The first production aircraft was delivered to the Japanese Defence Agency in by March 2005 61 F-2 fighters had been delivered. The aircraft are being assembled at Mitsubishi's Komaki South Plant in Nagoya. MHI expects to complete deliveries of 76 aircraft in the near future.

In June 2007, the F-2 made its first overseas deployment to Andersen AFB in Guam for joint US / Japan exercises. The F-2 dropped live weapons for the first time during the exercises.

F-2 fighter design
Kawasaki is responsible for the construction of the midsection of the fuselage, and also the doors to the main wheel and the engine. Mitsubishi builds the forward section of the fuselage and the wings.

Mitsubishi has also designed the lower-wing box structure, which includes lower skin, spars, ribs and cap, and is made from graphite-epoxy composite and co-cured together in an autoclave. This is the first application of co-cured technology to a production tactical fighter.

Fuji manufactures the upper-wing surface skin, the wing fairings, the radome, flaperons and the engine air-intake units and the tail section. Lockheed Martin Aeronautics Company supplies the rear section of the fuselage, the port-side wing boxes and the leading-edge flaps.

Cockpit
The cockpit is equipped with three multifunction displays, including a liquid crystal display from Yokogawa. The pilot's head-up display was developed by Shimadzu.

Integrated weapons system
The aircraft's integrated electronic warfare system, mission computer and active phased array radar were developed by Mitsubishi Electric.

An M61A1 Vulcan 20mm multi-barrel gun is installed in the wing root of the port wing. There are 13 hardpoints for carrying weapon systems and stores: one on the fuselage centreline, one on each wing-tip and five under each wing. The stores management system is supplied by Lockheed Martin.

There are two Frazer Nash common rail launchers manufactured by Nippi. The aircraft is capable of deploying the Raytheon AIM-7F/M medium-range Sparrow air-to-air missile, the Raytheon AIM-9L short-range Sidewinder and the Mitsubishi Heavy Industries AAM-3 short-range air-to-air missile.

The F-2 is armed with the ASM-1 and ASM-2 anti-ship missiles. Mitsubishi started developing the Type 80 series anti-ship missiles, ASM-1 and ASM-2, in 1980, originally for the F-1 fighter.

The fighter aircraft can also carry 500lb bombs, CBU-87/B cluster bombs and rocket launchers. The centreline and the inner-wing hardpoints can carry drop tanks with a 4,400kg fuel capacity.

"In June 2007, the F-2 made its first overseas deployment to Andersen AFB in Guam for joint US / Japan exercises."
Avionics and flight controls
Lockheed Martin is responsible for the avionics systems. The aircraft's digital fly-by-wire system has been developed by Japan Aviation Electric and Honeywell (formerly Allied Signal) under a joint development agreement.

The fly-by-wire modes include control augmentation, static stabilisation and load control during manoeuvres.

Communications
The communications systems fitted in the F-2 are the AN/ARC-164 transceiver, operating at UHF band and supplied by Raytheon, a V/UHF transceiver supplied by NEC, a Hazeltine information friend or foe interrogator, and an HF radio, developed and supplied by Kokusai Electric.

Turbofan engine
The aircraft is equipped with a General Electric F110-GE-129 afterburning turbofan engine. The engine develops 131.7kN and the speed of the aircraft is Mach 2. The F-2 produces 17,000lb of thrust, with 29,000lb with afterburners
F-2 Attack Fighter - Airforce Technology



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More Details:
Lockheed & Mitsubishi’s F-2 Fighter Partnership

Mitsubishi F-2 » Fighter Aircraft
 
JASDF F-2 Fighter

Key Data

  • Wingspan 10.8m
  • Span of Tailplane 6.05m
  • Length 15.52m
  • Height 4.96m
  • Empty Weight 12,000kg
  • Internal Fuel Capacity 3,600kg
  • Maximum Speed Mach 2
The F-2 support fighter aircraft is a multi role single engine fighter aircraft principally designed for the Japan Air Self Defence Force (JASDF), the result of a joint Japan and USA development programme. Mitsubishi Heavy Industries (MHI) is the prime contractor and Lockheed Martin Aeronautics Company serves as the principal US subcontractor. The F-2A is the single-seat version and F-2B is the two-seat version.

The Japanese Defence Agency originally planned to procure a total of 130 F-2 aircraft (83 single-seat and 47 two-seat aircraft) with deliveries to beyond 2010, but, in early 2007, this number was reduced to 94.

"The F-2 fighter aircraft can also carry 500lb bombs, CBU-87/B cluster bombs and rocket launchers."
The initial order was for 81 aircraft. A further five were ordered in March 2007 in a $150m contract. MHI awarded a further $250m contract to Lockheed Martin in April 2008 to manufacture components for eight more F-2 aircraft. The contract was the 12th annual contract awarded by MHI to Lockheed Martin.

F-2 fighter programme and development
In 1987, the JASDF selected a variant of the F-16C as the Japanese FS-X aircraft to replace the Mitsubishi F-1 aircraft, and in 1988 Mitsubishi was selected as prime contractor for the aircraft, which became known as the F-2. The programme involved technology transfer from the USA to Japan, and responsibility for cost sharing was split 60% by Japan and 40% by USA.

Four flying prototypes were developed, along with two static prototypes for static testing and for fatigue tests. Flight trials of the prototypes were successfully completed by 1997, and the aircraft entered production in 1998.

The first production aircraft was delivered to the Japanese Defence Agency in by March 2005 61 F-2 fighters had been delivered. The aircraft are being assembled at Mitsubishi's Komaki South Plant in Nagoya. MHI expects to complete deliveries of 76 aircraft in the near future.

In June 2007, the F-2 made its first overseas deployment to Andersen AFB in Guam for joint US / Japan exercises. The F-2 dropped live weapons for the first time during the exercises.

F-2 fighter design
Kawasaki is responsible for the construction of the midsection of the fuselage, and also the doors to the main wheel and the engine. Mitsubishi builds the forward section of the fuselage and the wings.

Mitsubishi has also designed the lower-wing box structure, which includes lower skin, spars, ribs and cap, and is made from graphite-epoxy composite and co-cured together in an autoclave. This is the first application of co-cured technology to a production tactical fighter.

Fuji manufactures the upper-wing surface skin, the wing fairings, the radome, flaperons and the engine air-intake units and the tail section. Lockheed Martin Aeronautics Company supplies the rear section of the fuselage, the port-side wing boxes and the leading-edge flaps.

Cockpit
The cockpit is equipped with three multifunction displays, including a liquid crystal display from Yokogawa. The pilot's head-up display was developed by Shimadzu.

Integrated weapons system
The aircraft's integrated electronic warfare system, mission computer and active phased array radar were developed by Mitsubishi Electric.

An M61A1 Vulcan 20mm multi-barrel gun is installed in the wing root of the port wing. There are 13 hardpoints for carrying weapon systems and stores: one on the fuselage centreline, one on each wing-tip and five under each wing. The stores management system is supplied by Lockheed Martin.

There are two Frazer Nash common rail launchers manufactured by Nippi. The aircraft is capable of deploying the Raytheon AIM-7F/M medium-range Sparrow air-to-air missile, the Raytheon AIM-9L short-range Sidewinder and the Mitsubishi Heavy Industries AAM-3 short-range air-to-air missile.

The F-2 is armed with the ASM-1 and ASM-2 anti-ship missiles. Mitsubishi started developing the Type 80 series anti-ship missiles, ASM-1 and ASM-2, in 1980, originally for the F-1 fighter.

The fighter aircraft can also carry 500lb bombs, CBU-87/B cluster bombs and rocket launchers. The centreline and the inner-wing hardpoints can carry drop tanks with a 4,400kg fuel capacity.

"In June 2007, the F-2 made its first overseas deployment to Andersen AFB in Guam for joint US / Japan exercises."
Avionics and flight controls
Lockheed Martin is responsible for the avionics systems. The aircraft's digital fly-by-wire system has been developed by Japan Aviation Electric and Honeywell (formerly Allied Signal) under a joint development agreement.

The fly-by-wire modes include control augmentation, static stabilisation and load control during manoeuvres.

Communications
The communications systems fitted in the F-2 are the AN/ARC-164 transceiver, operating at UHF band and supplied by Raytheon, a V/UHF transceiver supplied by NEC, a Hazeltine information friend or foe interrogator, and an HF radio, developed and supplied by Kokusai Electric.

Turbofan engine
The aircraft is equipped with a General Electric F110-GE-129 afterburning turbofan engine. The engine develops 131.7kN and the speed of the aircraft is Mach 2. The F-2 produces 17,000lb of thrust, with 29,000lb with afterburners
F-2 Attack Fighter - Airforce Technology



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More Details:
Lockheed & Mitsubishi’s F-2 Fighter Partnership

Mitsubishi F-2 » Fighter Aircraft





I long someday to see Pakistani F-16s in joint patrols with the JASDF's F-2s.

Is it wrong to dream of this ? I think not.

Such beautiful birds....
 
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