F-16 E/F Block 60 Desert Falcon

For a long time, it was uncertain if there would be a Block 60/62 version of the F-16C/D. However, in 1994 the United Arab Emirates (UAE) indicated that they needed 80 long-range strike fighters. The UAE wanted the latest available technology incorporated into these planes, and they indicated that if the USA was not willing to release such technologies, they might consider such competitors as the Eurofighter and the Dassault Rafale.

In pursuit of the UAE contract, Lockheed Martin came up with a delta-winged design based largely on the F-16XL. Wingroot troughs could hold four AIM-120 AMRAAM missiles, and a thrust-vectoring General Electric F110 engine was proposed. The delta-winged F-16 was to carry an improved radar, an internal FLIR and laser designation system, and an improved cockpit with a much more advanced set of multi-function and liquid-crystal displays.

However, very early on Lockheed Martin began to develop second thoughts about such an advanced aircraft, and began to consider a more conventional design for the UAE. The UAE had indicated that they were reluctant to commit themselves to an untried aircraft, one which had no other customers and in particular one in which the USAF was uninterested. By this time, the Pentagon had indicated that they were interested in the Joint Advanced Strike Technology (JAST) project as a potential replacement for the F-16. Lockheed Martin was a contender for the JAST project, and since the delta-winged F-16 could outperform the JAST in virtually every aspect except stealth and for considerably less money, the company might end up competing against itself. The delta-winged F-16 project was quietly shelved.

Lockheed then proposed a Block 60/62 lot of F-16C/Ds for the UAE order. The Block 60/62 would be largely based on the earlier Block 50/52, but would have an internal targeting and navigation system similar to LANTIRN but with only the sensor heads outside the aircraft. However, the Block 60/62 designation would not be applied until the aircraft actually enter production.

Again, two alternative engines would be offered. The Block 60 would be powered by the General Electric F110-GE-129EFE (Enhanced Fighter Engine), which would offer 34,000 lb.s.t with possible growth to 36,000 lb.s.t. The Block 62 would be powered by the Pratt & Whitney F100-PW-229A which offers 32,000 lb.s.t, with possible growth to 35,900 lb.s.t. Both of these engines are available with thrust vectoring.

The Block 60/62 will be equipped with a Northrop Grumman sensor suite that will be based on the APG-68(V)5 radar. It is an integrated system that will have an internal targeting and navigation system similar to LANTIRN but with only the sensor heads outside the aircraft. The Northrop Grumman AN/APG-80 Agile Beam Radar (ABR) will be provided which will have an active array with a large number of transmit/receive modules This beam can be steered almost instantaneously, making it possible to interleave various radar modes. For example, the radar could search for surface targets and do terrain-following while simultaneously searching for airborne threats.

The cockpit will have the backup electromechanical instruments removed, and three full-color displays will be added.

An attempt will be made to use commercially-available products such as PowerPC and Pentium processors, and the Ethernet databus will be used.

After two years of negotiations (including a controversy of whether computer software codes would be released), the UAE signed contracts on March 5, 2000 for 55 single seat and 25 two-seat Block 60 F-16s. These planes would be known as Desert Falcon. On March 14, it was announced that the powerplant would be the General Electric F110-GE-132, an uprated version of the existing F-16 engine which can deliver 32,000 lb.s.t.

The Block 60 also includes new conformal fuel tanks which significantly extend the aircraft’s range, with less drag than underwing drop tanks.

In 2003, the Block 60 was redesignated F-16E/F, in recognition of the major structural, avionics and propulsion system advancements, which make the Block 60 a practically new version of the F-16. They are also known as “Desert Falcons”, in recognition of their first customer.

The first of 80 Block 60 F-16s for the United Arab Emirates Air Force made its maiden flight at Fort Worth on December 6, 2003. It bore the serial 3001 and wore the civil registration of N161LM. Flight testing by Lockheed Martan began in early 2004.

Source joebaugher.com


UAEAF Inventory

Program Model Block Qty. Serials Delivered
Initial Order F-16E Block 60 55 3026/3080 2004-2006
F-16F Block 60 25 3001/3025 2003-2006

Source f-16.net

The most advanced F-16s in the world aren’t American. That distinction belongs to the UAE, whose F-16 E/F Block 60s are a half-generation ahead of the F-16 C/D Block 50/52+ aircraft that form the backbone of the US Air Force, and of many other fleets around the world. The Block 60 has been described as a lower-budget alternative to the F-35A Joint Strike Fighter, and there’s a solid argument to be made that their performance figures and broad sensor array will even keep them ahead of pending F-16 modernizations in countries like Taiwan, South Korea, and Singapore.

See details of F-16C/D: HERE

The UAE invested in the “Desert Falcon’s” development, and the contract reportedly includes royalty fees if other countries buy it. Investment doesn’t end when the fighters are delivered, either. Money is still needed for ongoing training, fielding, and equipment needs – and the UAE has decided that they need more planes, too. This DID article showcases the F-16 Block 60/61, and offers a window into its associated costs and life cycle, including dedicated equipment purchases for this fighter fleet.

UAE Defence Ministry enters $1.6 billion deal with Lockheed Martin to upgrade F-16 fighters

DUBAI (Reuters) – United Arab Emirates’ Defence Ministry announced a 6 billion dirham (1.24 billion pounds) deal with Lockheed Martin Corp (LMT.N) to upgrade F-16 jet fighters, a spokesman said on Sunday.

The deal is to upgrade 80 F-16 jet fighters, Major General Abdullah Al Sayed Al Hashemi, Chief of the Military Committee and the spokesman of the UAE Armed Forces, told a news conference. Source reuters.com

The F-16E/F “Desert Falcon”

The F-16 has become what its designers intended it to be: a worthy successor to the legendary P-51 Mustang whose principles of visibility, agility, and pilot-friendliness informed the Falcon’s original design. The planes have been produced in several countries around the world, thanks to licensing agreements, and upgrades have kept F-16s popular. It’s no exaggeration to call the F-16 the defining fighter of its age, the plane that many people around the world think of when they think “fighter.” They remain the American defense industry’s greatest export success story of the last 40 years, but the aircraft’s ability to handle future adversaries like the thrust-vectoring MiG-29OVT/35 and advanced surface-air missile systems is now in question.


The F-16 has now undergone 6 major block changes since its inception in the late 1970s, incorporating 4 generations of core avionics, 5 engine versions divided between 2 basic models (P&W F100 and GE F110), 5 radar versions, 5 electronic warfare suites, and 2 generations of most other subsystems. Moore’s Law applies as well, albeit more slowly: the latest F-16’s core computer suite has over 2,000 times the memory, and over 260 times the throughput, of the original production F-16.

Block 60: Technical

Each new iteration of the fighter costs money to develop, integrate, and test. The UAE invested almost $3 billion into research and development for the F-16 E/F Block 60 Desert Falcon. First flight took place in December 2003, and flight testing by Lockheed Martin began in early 2004. UAE pilot training on the F-16E/F began at Tucson Air National Guard Base, AZ in September 2004, and the first group of pilots completed their training in April 2005. The first Desert Falcons arrived in the UAE in May 2005.


All of the initial 60 aircraft have been delivered, and all training now takes place in the UAE. Versions of this aircraft have been entered in a number of international export competitions as well, including Brazil’s F-X2 (eliminated) and India’s MMRCA (eliminated), but it hasn’t found any buyers yet. Production will restart soon anyway, thanks to the UAE’s impending add-on buy 30 F-16 E/F Block 61s with minor component upgrades.

The aircraft’s advanced avionics suite has room available for future improvements. The Block 60’s modular mission computer has a processing throughput of 12.5 million instructions per second and provides sensor and weapons integration.

The ALQ-165 electronic countermeasures system, also known as the Airborne Self-Protection Jammer (ASPJ), is a sophisticated, high-power jamming system developed to fulfill both U.S. Navy and Air Force requirements – although the USAF abandonned the program a while ago. Missile warning systems on the Block 60 provide advanced warning of approaching missiles so the pilot can activate countermeasures in time. The Block 60 F-16 can accommodate both active and passive missile warning systems currently under development. Source f-16.net

AN/ALQ-165 Airborne Self-Protection Jammer (ASPJ)


The ASPJ contributes to full-dimensional protection by improving individual aircraft probability of survival. The AN/ALQ-165 ASPJ is an automated modular reprogrammable active radar frequency (RF) deception jammer designed to contribute to the electronic self protection of the host tactical aircraft from a variety of air to air and surface to air RF threats. The ASPJ was designed to accomplish threat sorting, threat identification, and jamming management in a dense signal environment to counter multiple threats. The modular architecture supports internal integration with other avionics/weapons systems in a variety of aircraft. The ALQ-165, a joint venture between Northrop Grumman and ITT Avionics, is now in production for the US Marine Corps and Navy’s F/A-18s and F-14. Source fas.org

Design & Powerplant

The aircraft’s conformal fuel tanks (CFTs) let them carry more fuel, with less drag than underwing drop tanks. All that fuel feeds GE’s new F110-GE-132 engine, which produces up to 32,500 pounds of thrust to offset the plane’s increased weight. The -132 is a derivative of the proven F110-GE-129, a 29,000-pound thrust class engine that powers the majority of F-16 C/D fighters worldwide. Even with a bigger engine and more weight from added sensors, CFTs, etc., Block 60 fighters offer a mission radius of 1,025 miles – a 40% range increase over F-16s without CFTs.


Conformal fuel tanks (CFTs)

F-16UAE11Conformal fuel tanks (CFTs) let them carry more fuel, with less drag than underwing drop tanks

GE’s new F110-GE-132 engine

p0583600GE’s new F110-GE-132 engine, which produces up to 32,500 pounds of thrust

The F110 was developed utilizing the same core design of the F101 engine. This engine has different fan and afterburner packages to tailor engine performance compared with the F101 engine.

The F110-GE-132 is the latest and most advanced member of the F110 engine family yielding 32,000 pounds of thrust. Derived from the F110-GE-129, this engine incorporates some advanced technologies related to both the F414 and F120 engines. As a result of that, -132 has an increased combat performance over -129 and lower total ownership costs.

The F110-GE-132 utilizes General Electric Aircraft Engines (GEAE)’s extensive technology base, including: a long-chord blisk fan derived from the F118 engine, a radial afterburner derived from the F414 engine and enhanced for the F136 engine (Joint Strike Fighter), and a composite outer duct based on the F404 and F414 engines. In the future, GEAE plans to infuse a new core developed to extend the service life of the engine thus increasing durability and time on wing.

The F110-GE-132 engine was developed to power the F-16C/D Block 60 or F-16E/F aircraft ordered by the United Arab Emirates (UAE) Air Force.


  • Fan Diameter: 1,170 millimeter
  • Length: 4.60 meter


  • Dry Weight: 1,819 kilogram (4,010 pound)
  • Thrust: 32,500 pound (14,742 kilogram)

Source deagel.com

Conformal tanks aren’t exclusive to the Block 60. They’re options for many F-16 variants, and can be removed before missions, but that may not be a great idea for the UAE’s fleet. It’s a classic give/take scenario, in which more capability (q.v. electronics) means more weight, which requires a larger engine, which shortens range without more fuel. The conformal tanks more than make up that difference, creating a formidable strike fighter, but they exact their own aerodynamic cost in acceleration and handling. That tradeoff hurt attempts to export the fighter to India’s IAF, which prioritized maneuvering performance and left the Desert Falcon off of their shortlist.



AN/APG-80 AESA radar


AN/APG-80 is Northrop-Grumman’s AESA radar which developed for export with F-16E/F block 60 and intended for 4th gen. fighters modernization programs too. In comparison with older slotted array F-16C/D radar AN/AGP-68(V)7 the range of fly target detection is as twice as longer while synthetic aperture mode is added for ground strike capability.

Style of antenna:

  • APG-80: AESA, 1,000 T/R

Effective tracking range for RCS = 1 m2 target

  • APG-80: 110~120 km

Horizontal tracking angles

  • APG-80: +/- 60 degrees

Target number of TWS at the same time:

  • APG-80: 20 (now) ~ 50 (potential in the future) targets

Performing A-A and A-G modes at the same time:

  • APG-80: Yes

LPI capability:

  • APG-80: Yes

High speed capability of Data-link/communication:

  • APG-80: No

Advanced functions for Microwave-weapon / CPU virus spreader/ Net-Hacker:

  • APG-80: No

MTBF (mean time between failures)

  • APG-80: 500~800 hrs

Source igorrgroup.blogspot.com

Example Radar Cross Section Range
AA-missile 0.0001 m² > 11 km
stealth fighter 0.001 m² > 20 km
cruise missile 0.1 m² > 62 km
classic fighter 1.0 m² > 110 km
bomber 5.0 m² > 165 km
passenger aircraft 10.0 m² > 195 km

Source radartutorial.eu

The Desert Falcons’ most significant changes are electronic. Northrop Grumman’s AN/APG-80 AESA radar is the most significant advance, and made the UAE the first fighter force in the world to field this revolutionary new radar technology outside of the USA. Compared to mechanically-scanned arrays like the AN/APG-68v9s that equip advanced American and foreign F-16s, AESA radars like the APG-80 have more power, better range, less sidelobe “leakage,” near-100% combat availability, and more potential add-on capabilities via software improvements. Unlike the APG-68s, the APG-80 can perform simultaneous ground and air scan, track, and targeting, and it adds an “agile beam” that reduces the odds of detection by opposing aircraft when the radar is on.

This last feature is important. Seeing the enemy first remains every bit as significant as it was in Boelcke’s day, but the inverse square law for propagation means that turning on older radar design is like activating a flashlight in a large and dark building. It can be seen much farther away than it can illuminate. An agile-beam AESA radar largely negates that disadvantage, while illuminating enemies who may not have their own radars on.

United Arab Emirates (UAE) F-16 get Modernizing head-up displays

Digital Light Engine Head-Up Display (HUD)

See thru display for Military Aviation

BAE Systems has been a leader in HUD development and production for more than 50 years, a position gained through continuous investment in technology and innovation. BAE Systems:

  • has produced over 14,000 head-up displays
  • that are in service on over 50 different aircraft types
  • and for more than 50 countries


  • Better situational awareness for the military aviator
  • Allows some freedom of head movement, reducing pilot fatigue
  • Backward compatible to any existing aircraft interface which offers minimal impact on display performance

Photo of the Digital Light Engine Head-Up Display

Designed for mission effectiveness, the DLE HUD has addressed obsolescence issues by:

  • removing the conventional cathode ray tube (CRT) technology powering the display and
  • introducing a more advanced digital display solution

With more military aircraft upgrade advancements to digital display solutions, the DLE HUD offers easy integration into existing HUD space. Offering more than 20 percent life cycle cost reduction and at least four times greater Mean Time Between Failure (MTBF), the DLE HUD is a future proof investment in the advanced display technology segment.

Typical performance specification

Specification Display Source Analogue Symbol Generator, EU, AEU, MLU, IMDC
Display Surface Resolution 1280 x 1024 pixels
Field of View 25° x 22°
Display Luminance 0 to > 2000 ftL
Luminance Uniformity < 20% within a 10° diameter area
< 30% over the TFoV
Secondary Images < 2% of primary
Display Contrast > 1.2:1 against an ambient of 10,000 ftL
> 1200:1 Sequential
Outside World Transmission > 75%
Image Positional Accuracy < 0.8mR error within 5° of CFoV < 1mR elsewhere within FoV
Mass < 20.1 Kilograms (ballast may be applied to maintain C of G position if required)
Operating Temperature -40°C to +75°C
Storage Temperature -40°C to +85°C
Operating Altitude 0 to 70,000 ft
Latency <1mS
Dimensions Form Fit Function

Source baesystems.com

FLIR targeting system (IFTS)


The planned under-nose integrated FLIR targeting system (IFTS) has been replaced by a new podded FLIR mounted on the intake hardpoints. Apparently, there were problems in achieving the promised performance with the original layout. The Northrop Grumman AAQ-32 targeting FLIR and laser designator has been repackaged in a new station. However, the original wide-area navigation FLIR housing above the nose will still be there. Source joebaugher.com

Northrop Grumman AAQ-32 targeting FLIR and laser designator


The IFTS provides 24-hour precision strike and navigation capabilities. It detects and identifies both ground and airborne targets, even at night or in adverse weather, for highly accurate weapons delivery. Source northropgrumman.com

AN/AAQ-32 IFTS Laser Designator

General data:
Type: Laser Designator Altitude Max: 0 m
Range Max: 27.8 km Altitude Min: 0 m
Range Min: 0 km Generation: Not Applicable (N/A)
Sensors / EW:
AN/AAQ-32 IFTS [Laser Designator] – Laser Designator
Role: Laser Target Designator & Ranger (LTD/R)
Max Range: 27.8 km

AN/AAQ-32 IFTS Infrared

General data:
Type: Infrared Altitude Max: 0 m
Range Max: 83.3 km Altitude Min: 0 m
Range Min: 0 km Generation: Infrared, 3rd Generation Imaging (2000s/2010s, Impr LANTIRN, Litening II/III, ATFLIR)
Properties: Identification Friend or Foe (IFF) [Side Info], Classification [Class Info] / Brilliant Weapon [Automatic Target Aquisition], Continous Tracking Capability [Visual]
Sensors / EW:
AN/AAQ-32 IFTS [FLIR] – Infrared
Role: Infrared, Attack FLIR
Max Range: 83.3 km

The Desert Falcons also take a step beyond the standard ground surveillance and targeting pod systems fielded on other F-16s, by incorporating them into the aircraft itself. Northrop Grumman’s AN/ASQ-32 IFTS is derived from its work on the AN/AQS-28 LITENING AT, but internal carriage reduces drag and radar signature, and frees up a weapons pylon. The ASQ-32 can even be used to find aerial targets, allowing passive targeting, and offering a tracking option that radar stealth won’t evade.

Joint Helmet Mounted Cueing System (JHMCS)


In an air-to-air role, the JHMCS, combined with the AIM-9X missile, form the High-Off-BoreSight (HOBS) system. HOBS is an airborne weapon-interception system that enables pilots to accurately direct or “cue” onboard weapons against enemy aircraft merely by pointing their heads at the targets to guide the weapons, while performing high-G aircraft maneuvers that may be required to complete the attack.

In an air-to-ground role, the JHMCS is used in conjunction with targeting sensors (radar, FLIR, etc.) and “smart weapons” to accurately and precisely attack surface targets. It allows F-15E aircrew to provide unparalleled support to ground troops in the CAS environment.

In all roles, the JHMCS provides the pilot with aircraft performance, targeting, weaponry and threat warning information, regardless of where the pilot is looking, significantly enhancing pilot situation awareness throughout the mission. In a dual-seat aircraft, each crewmember can wear a JHMCS helmet, perform operations independent of each other, and have continuous awareness of where the other crewmember is looking.

System Features

Unlike one of its predecessor, the DASH system, which is integrated into the helmet itself, JHMCS is a clip-on attachment unit, which can be latched into position with one hand during flight (see photo below). It fits to modified HGU-55/P, HGU-56/P or HGU-68/P helmets and it features a newer, faster digital processing package than that used in the DASH. The overall design is more advanced than DASH, based on the collective knowledge accumulated by Elbit and Kaiser through the years.


The JHMCS has a magnetic helmet-mounted tracker (like DASH), which determines where the pilot’s head is pointed, combined with a miniature display system that projects information onto the pilot’s visor. A magnetic transmitter unit is fixed to the pilot’s seat and a magnetic field probe is mounted on the helmet to determine where the helmet is actually pointing. A Helmet Vehicle Interface ( HVI) interacts with the aircraft system bus to provide signal generation for the helmet display. The head tracker and visor display together act as a targeting device that can aim sensors and weapons.

To obtain a variety of information and sensor-based data pilots can refer to the visual display on the inside of the helmet while remaining in a “heads-up” or “outside” position during combat; this eliminates the break in visual contact that occurs when they look away to check the display readouts in the cockpit. This significantly improves pilot situational awareness during all mission elements. The visor display presents monochrome calligraphic symbology (stroke display) with information like airspeed, altitude, G-load, AoA, target range, targeting cues, threat warnings, etc. JHMCS provides support for raster scanned imagery to display FLIR or IRST pictures for night operations and provides collimated symbology and imagery to the pilot. JHMCS symbology covers a 20 degree field of view for the right eye, with an 18 mm exit pupil (see photo below).

To aim and fire a missile, pilots simply move their heads to align a targeting cross (placed in the middle of the projected imagery) with the target and press a switch on the flight controls to direct and fire a weapon.

aug_i_ttImage: boeing.com

To attack a ground target, the pilot can acquire the target with a sensor and note it’s location on the helmet display. Alternatively, the pilot can use the helmet display to cue sensors and weapons to a visually detected ground target. Note that precision ordnance cannot be released based on JHMCS targeting alone, the system is not accurate enough for this. However it can be used to direct the aircraft’s much more precise targeting systems (targeting pod) towards the target the pilot is looking at. This way the tedious “soda-straw” search limited to a display image generated by the narrow field of view targeting system can be shortened significatly. With JHMCS, target acquisition can follow a much quicker “look, sharpen, shoot” process.

The system can be used without requiring the aircraft to be maneuvered, significantly reducing the time needed to prosecute an attack, which also minimizes the time spent in the threat environment.

Since targets may be located at high-off-boresight line-of-sight locations in relation to the shooter, the system delivers a short-range intercept envelope that is significantly larger than any other air-to-air weapon in use. When combined with the AIM-9X missile, JHMCS allows effective target designation up to 80 degrees either side of the aircraft’s nose.

The JHMCS display assembly requires two cable connections: a high voltage power cable for operation and a data cable for information exchange with the host aircraft. Unlike in DASH the high voltage power supply is not embedded in the helmet, it feeds up via an umbilical, through a quick disconnect inline high coltage rated connector.

When used in conjunction with a datalink, the system permits handoff of visually detected targets from one aircraft to another, with the second aircraft receiving visual cueing to the target. Source f-15e.info

A JHMCS helmet mounted display provides parity with the fighter’s most modern counterparts, and displays information from the aircraft’s radar and sensors wherever the pilot looks. Its real advantage is that it creates a much larger targeting zone, which can be fully exploited by the newest air-to-air missiles like the AIM-9X. Avionics improvements round out the enhancements via an advanced mission computer to enhance sensor and weapon integration, a trio of 5″x7″ color displays in the cockpit, etc.

Avionics improvements round out the enhancements via an advanced mission computer to enhance sensor and weapon integration, a trio of 5″x7″ color displays in the cockpitf_16e_block_60_landing_approach_to_tanagra_by_roen911-d5nyf2oRear seat F16F

Various advanced electronic countermeasures systems make up the Falcon Edge Integrated Electronic Warfare System (IEWS), which provides both advance warning capabilities and automatic countermeasures release.



F-16s have an extremely wide range of integrated weapons, but Mideast politics has kept some American weapons from the UAE’s hands. Their Desert Falcons won’t carry the same stealthy AGM-158 JASSM long-range, stealthy cruise missiles found on American F-16s, for instance. Nor can they carry the similar “Black Shahine” MBDA Storm Shadow derivatives that equip the UAE’s Mirage 2000 fleet.

Mirage 2000: Details

p1473919080-5.jpgMirage 2000-9EAD – UAE – Image: Digital Photography Review10108929b

20mm General Electric M61A1 multi-barrel cannon

Image: f-16.net


slam-er_graphicGPS/IIR-guided AGM-84H SLAM-ER cruise missiles that can deliver accurate hits on ships and land targets up to 250 km away – UAE have received this weapon since 2013

The SLAM-ER (Expanded Response) Block 1F, a major upgrade to the SLAM missile that is currently in production, provides over twice the missile range, target penetration capability, and control range of SLAM. SLAM-ER has a greater range (150+ miles), a titanium warhead for increased penetration, and software improvements which allow the pilot to retarget the impact point of the missile during the terminal phase of attack (about the last five miles). In addition, many expansions are being made to improve performance, survivability, mission planning, and pilot (man-in-the-loop) interface. The SLAM-ER development contract was awarded to McDonnell Douglas Aerospace (Now BOEING) in February of 1995. SLAM-ER achieved its first flight in March of 1997. All Navy SLAM missiles are currently planned to be retrofitted to SLAM-ER configuration. About 500 SLAM missiles will be converted to the SLAM-ER configuration between FY 1997 and FY 2001. Source fas.org


AGM-154_Joint_Standoff_Weapon_MainStealthy AGM-154C JSOW glide bombs

The AGM-154A (Formerly Advanced Interdiction Weapon System) is intended to provide a low cost, highly lethal glide weapon with a standoff capability. JSOW family of kinematically efficient, air-to-surface glide weapons, in the 1,000-lb class, provides standoff capabilities from 15 nautical miles (low altitude launch) to 40 nautical miles (high altitude launch). The JSOW will be used against a variety of land and sea targets and will operate from ranges outside enemy point defenses. The JSOW is a launch and leave weapon that employs a tightly coupled Global Positioning System (GPS)/Inertial Navigation System (INS), and is capable of day/night and adverse weather operations.

The JSOW uses inertial and global positioning system for midcourse navigation and imaging infra-red and datalink for terminal homing. The JSOW is just over 13 feet in length and weighs between 1000-1500 pounds. Extra flexibility has been engineered into the AGM-154A by its modular design, which allows several different submunitions, unitary warheads, or non-lethal payloads to be carried. The JSOW will be delivered in three variants, each of which uses a common air vehicle, or truck, while substituting various payloads.

AGM-154A (Baseline JSOW) The warhead of the AGM-154A consists of 145 BLU-97/B submunitions. Each bomblet is designed for multi-target in one payload. The bomblets have a shaped charge for armor defeat capability, a fragmenting case for material destruction, and a zirconium ring for incendiary effects.

AGM-154B (Anti-Armor) The warhead for the AGM-154B is the BLU-108/B from the Air Force’s Sensor Fuzed Weapon (SFW) program. The JSOW will carry six BLU-108/B submunitions. Each submunition releases four projectiles (total of 24 per weapons) that use infrared sensors to detect targets. Upon detection, the projectile detonates, creating an explosively formed, shaped charge capable of penetrating reinforced armor targets.

AGM-154C (Unitary Variant) The AGM-154C will use a combination of an Imaging Infrared (IIR) terminal seeker and a two-way data link to achieve point target accuracy through aimpoint refinement and man-in-the-loop guidance. The AGM-154C will carry the BLU-111/B variant of the MK-82, 500- pound general purpose bomb, equipped with the FMU-152 Joint Programmable Fuze (JPF) and is designed to attack point targets. Source fas.org

GBU-39 Small Diameter Bombs

GBU-39 Small Diameter Bombs

On the other hand, the Desert Falcons’ array of integrated weapons will include medium range, GPS/IIR-guided AGM-84H SLAM-ER cruise missiles that can deliver accurate hits on ships and land targets up to 250 km away. At shorter ranges, stealthy AGM-154C JSOW glide bombs and GBU-39 Small Diameter Bombs give them wide-ranging one-pass attack capabilities against hard targets. In the air, AIM-9X Block II Sidewinder short-range missiles give them over-the-shoulder kill capability, and a combat option that many of the UAE’s neighbors haven’t fielded yet.

AIM-9X Block II Sidewinder

aim9xAIM-9X Block II Sidewinder short-range missiles give them over-the-shoulder kill capability Image: donhollway.com

The current fifth-generation AIM-9X is to the old 9B what humans are to homo erectus. Paired with a pilot’s helmet-mounted display, it can “look” 90 degrees off-boresight for its target and, with three-dimensional vectored-thrust steering, turn 180 degrees in pursuit. One test pilot at Naval Air Station Fallon, Nev., freshly returned from getting every visual-range first-shot “kill” on Top Gun instructors in F-18s and F-14s, enthused, “If you have [a weapons-sight] helmet and AIM-9X, you are King Kong of the air.”

The latest versions have “lock-on after launch” capability, lending themselves to “cloud shooting,” 360-degree target selection via data link from aircraft other than the launching fighter. Source donhollway.com

Block 60: Political Issues

In the course of development, 2 key issues came up with respect to the F-16 Block 60. One was the familiar issue of source code control for key avionics and electronic warfare systems. The other was weapons carriage.

As a rule, the software source codes that program the electronic-warfare, radar, and data buses on US fighters are too sensitive for export. Instead, the USA sent the UAE “object codes” (similar to APIs), which allow them to add to the F-16’s threat library on their own.

The other issue concerned the Black Shahine derivative of MBDA’s Storm Shadow stealth cruise missile. The Missile Technology Control Regime (MTCR) defines 300 km as the current limit for cruise missiles, and the terms of the sale allow the United States to regulate which weapons the F-16s can carry. Since the Black Shahine was deemed to have a range of over 300 km, the US State Department refused to let Lockheed Martin change the data bus to permit the F-16E/Fs to carry the missile.

Black Shahine/MBDA’s Storm Shadow

Black Shahine derivative of MBDA’s Storm Shadow stealth cruise missile Since the Black Shahine was deemed to have a range of over 300 km, the US State Department refused to let Lockheed Martin change the data bus to permit the F-16E/Fs to carry the missile

Originated From: FranceUnited Kingdom

Possessed By: FranceGreeceItalySaudi ArabiaUnited Arab EmiratesUnited Kingdom

Alternate Name: Black Shahine

Class: Subsonic

Basing: Air-to-surface

Length: 5.1 m

Launch Weight: 1,300 kg

Payload: 400 kg

Warhead: Tandem HE (BROACH)

Propulsion: Turbojet

Range: 250-400 km

Status: Operational

In Service: 2004

Storm Shadow Cutaway with Annnotations MBDA UK Limited © Copyright 2011SCALP EG/Storm Shadow cruise missile.

In 1991, Matra (later Matra BAe Dynamics, MBDA) proposed a long-range, stand-off variant based on the APACHE design which would have a designated range of 600 km. This variant was originally known as APACHE C, later renamed to APTGD (Armement de Precision Tire á Grande Distance), and was finally deemed the SCALP (Systéme de Croisiére conventional Autonone á Longue Portée de precision). France adopted the SCALP EG (general purpose) variant in 1994. The SCALP EG, which is nearly identical to the Storm Shadow/Black Shaheen, went on to be the basis for the SCALP Naval version.

Due to its relation to the APACHE system, the specifications reflect many similarities. The SCALP EG/Storm Shadow is 5.1 m in length, 0.63/ 0.48 m in body width/height diameter, and 1,300 kg in launch weight. The payload is slightly less than the APACHE at 400 kg. The notable distinction between the APACHE and the SCALP/Storm Shadow missiles are the warhead types and the effective range. The SCALP carries a single HE penetrator warhead, making it a far more versatile system than the submunitions carried by the APACHE. Additionally, the range for the SCALP/Storm Shadow is 250 to 400 km — significantly further than the APACHE’s 140 km. Data missilethreat.com

The Mirage 2000-9 upgrades that the UAE developed with France addressed this issue, giving the UAE a platform capable of handling their new acquisition. As of 2013, UAE F-16E/F fighters have finally received the SLAM-ER precision attack missile, giving them the shorter-range but very accurate strike capabilities. Source: defenseindustrydaily.com

Updated Feb 12, 2018

YF-16 F-16A F-16C Block 30 F-16E Block 60


Length 48 ft 5 in (14.8 m) 49 ft 6 in (15.1 m) 49 ft 5 in (15.1 m) 49 ft 4 in (15.0 m)
Wingspan 31 ft 0 in (9.45 m) 31 ft 0 in (9.45 m) 31 ft 0 in (9.45 m) 31 ft 0 in (9.45 m)
Height 16 ft 3 in (4.95 m) 16 ft 8 in (5.08 m) 16 ft 8 in (5.08 m) 16 ft 8 in (5.08 m)
Empty weight 13,600 lb (6,170 kg) 16,300 lb (7,390 kg) 18,900 lb (8,570 kg) 22,000 lb (9,980 kg)
Maximum take-off weight 37,500 lb (17,000 kg) 42,300 lb (19,200 kg) 46,000 lb (20,900 kg)
Maximum speed

Mach 2.0

Combat radius 295 nmi (546 km)
Engine PW F100-PW-200 PW F100-PW-200 GE F110-GE-100 GE F110-GE-132
Thrust 23,800 lbf (106 kN) 23,800 lbf (106 kN) 28,600 lbf (127 kN) 32,500 lbf (145 kN)
Radar AN/APG-66 AN/APG-68 AN/APG-80

Source: wiki


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