Showing posts with label UAV. Show all posts
Showing posts with label UAV. Show all posts

Boeing Insitu ScanEagle

The Boeing Insitu ScanEagle is a small, low-cost, long-endurance unmanned aerial vehicle (UAV) built by Insitu, a subsidiary of Boeing. The ScanEagle was designed by Insitu based on the Insitu SeaScan, a commercial UAV that helped fishermen look for fish. The ScanEagle continues to be upgraded with improved technology and reliability.
ScanEagle is a descendant of another Insitu UAV, SeaScan, which was conceived of as a remote sensor for collecting weather data as well as helping commercial fishermen locate and track schools of tuna. ScanEagle emerged as the result of a strategic alliance between Boeing and Insitu. The resulting technology has been successful as a portable Unmanned Aerial System (UAS) for autonomous surveillance in the battlefield, and has been deployed since August 2004 in the Iraq War.
ScanEagle carries a stabilized electro-optical and/or infrared camera on a lightweight inertial stabilized turret system integrated with communications range over 62 miles (100 km), and flight endurance of 20+ hours. ScanEagle has a 10.2-foot (3.1 m) wingspan a length of 4.5 feet (1.4 m) and a mass of 44 pounds (20 kg) and can operate up to 80 knots (92 mph; 150 km/h), with an average cruising speed of 48 knots (55 mph; 89 km/h). Block D aircraft featured a higher-resolution camera, a custom-designed Mode C transponder and a new video system. A Block D aircraft, flying at Boeing's test range in Boardman, Oregon set a type endurance record of 22 hours, 8 minutes.
ScanEagle needs no airfield for deployment. Instead, it is launched using a pneumatic launcher, patented by Insitu, known as the "SuperWedge" launcher. It is recovered using the "Skyhook" retrieval system, which uses a hook on the end of the wingtip to catch a rope hanging from a 30-to-50-foot (9.1 to 15 m) pole. This is made possible by high-quality differential GPS units mounted on the top of the pole and UAV. The rope is attached to a shock cord to reduce stress on the airframe imposed by the abrupt stop.
Each ScanEagle system costs US$3.2 million (2006). A complete system comprises four air vehicles or AVs, a ground control station, remote video terminal, and the Skyhook launch and recovery system.
Improvements
On 18 March 2008, Boeing, with ImSAR and Insitu successfully flight-tested a ScanEagle with ImSAR's NanoSAR A radar mounted aboard. The ImSAR NanoSAR is the world's smallest Synthetic Aperture Radar, weighs 3.5 lb (1,590 g) and is 100 cubic inches (1.6 litres) in volume. It is designed to provide high quality real-time ground imaging through adverse weather conditions or other battlefield obscurants.
In 2009, Boeing and Insitu announced the NightEagle, a modified ScanEagle Block E with an infrared camera for night operations.
In August 2010, Boeing announced plans to control ScanEagles from control stations on E-3A AWACS aircraft and on the V-22.
In July 2011, a team of two ScanEagles and another UAV cooperated to search and navigate a mountain area autonomously.
Operational History
The ScanEagle entered service with the U.S. Navy in 2005. In addition to the United States military, the Australian Army also operates the ScanEagle UAV. As well the Canadian Government announced in August 2008 that they would lease the ScanEagle for use of their military operations in Afghanistan.
In April 2009, a ScanEagle launched by the U.S. Navy was used during the stand-off between the U.S. Navy and a lifeboat controlled by pirates holding Capt. Richard Phillips of the MV Maersk Alabama in the Indian Ocean after a failed hijack attempt.
Insitu announced that the ScanEagle had totaled 500,000 combat flight hours and over 56,000 sorties by July 2011.
In December 2012, Iran stated it had captured an American ScanEagle that allegedly violated its airspace over the Persian Gulf. Iran later stated it had also captured two other ScanEagles. The U.S. Navy stated that none of its ScanEagles were missing. Photo evidence of an ScanEagle in Iran showed no U.S. military markings. It was also reported that Iran is producing a copied version of the ScanEagle and has put that UAV into military service.
Specifications
General characteristics
Crew
none on-board
Length
3.9 feet (1.19 meters)
Wingspan
10.2 feet (3.1 meters)
Loaded Weight
39.7 lbs (18 kilograms)
Powerplant
1 × 3W 2-stroke piston engine, 1.5 hp

Performance
Maximum speed
55-80 mph
Endurance
20 + hours
Service ceiling
16,000 feet above ground level (4,876 meters)

Avionics
High resolution, day/night camera and thermal imager

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Boeing Insitu ScanEagle

The Boeing Insitu ScanEagle is a small, low-cost, long-endurance unmanned aerial vehicle (UAV) built by Insitu, a subsidiary of Boeing. The ScanEagle was designed by Insitu based on the Insitu SeaScan, a commercial UAV that helped fishermen look for fish. The ScanEagle continues to be upgraded with improved technology and reliability.
ScanEagle is a descendant of another Insitu UAV, SeaScan, which was conceived of as a remote sensor for collecting weather data as well as helping commercial fishermen locate and track schools of tuna. ScanEagle emerged as the result of a strategic alliance between Boeing and Insitu. The resulting technology has been successful as a portable Unmanned Aerial System (UAS) for autonomous surveillance in the battlefield, and has been deployed since August 2004 in the Iraq War.
ScanEagle carries a stabilized electro-optical and/or infrared camera on a lightweight inertial stabilized turret system integrated with communications range over 62 miles (100 km), and flight endurance of 20+ hours. ScanEagle has a 10.2-foot (3.1 m) wingspan a length of 4.5 feet (1.4 m) and a mass of 44 pounds (20 kg) and can operate up to 80 knots (92 mph; 150 km/h), with an average cruising speed of 48 knots (55 mph; 89 km/h). Block D aircraft featured a higher-resolution camera, a custom-designed Mode C transponder and a new video system. A Block D aircraft, flying at Boeing's test range in Boardman, Oregon set a type endurance record of 22 hours, 8 minutes.
ScanEagle needs no airfield for deployment. Instead, it is launched using a pneumatic launcher, patented by Insitu, known as the "SuperWedge" launcher. It is recovered using the "Skyhook" retrieval system, which uses a hook on the end of the wingtip to catch a rope hanging from a 30-to-50-foot (9.1 to 15 m) pole. This is made possible by high-quality differential GPS units mounted on the top of the pole and UAV. The rope is attached to a shock cord to reduce stress on the airframe imposed by the abrupt stop.
Each ScanEagle system costs US$3.2 million (2006). A complete system comprises four air vehicles or AVs, a ground control station, remote video terminal, and the Skyhook launch and recovery system.
Improvements
On 18 March 2008, Boeing, with ImSAR and Insitu successfully flight-tested a ScanEagle with ImSAR's NanoSAR A radar mounted aboard. The ImSAR NanoSAR is the world's smallest Synthetic Aperture Radar, weighs 3.5 lb (1,590 g) and is 100 cubic inches (1.6 litres) in volume. It is designed to provide high quality real-time ground imaging through adverse weather conditions or other battlefield obscurants.
In 2009, Boeing and Insitu announced the NightEagle, a modified ScanEagle Block E with an infrared camera for night operations.
In August 2010, Boeing announced plans to control ScanEagles from control stations on E-3A AWACS aircraft and on the V-22.
In July 2011, a team of two ScanEagles and another UAV cooperated to search and navigate a mountain area autonomously.
Operational History
The ScanEagle entered service with the U.S. Navy in 2005. In addition to the United States military, the Australian Army also operates the ScanEagle UAV. As well the Canadian Government announced in August 2008 that they would lease the ScanEagle for use of their military operations in Afghanistan.
In April 2009, a ScanEagle launched by the U.S. Navy was used during the stand-off between the U.S. Navy and a lifeboat controlled by pirates holding Capt. Richard Phillips of the MV Maersk Alabama in the Indian Ocean after a failed hijack attempt.
Insitu announced that the ScanEagle had totaled 500,000 combat flight hours and over 56,000 sorties by July 2011.
In December 2012, Iran stated it had captured an American ScanEagle that allegedly violated its airspace over the Persian Gulf. Iran later stated it had also captured two other ScanEagles. The U.S. Navy stated that none of its ScanEagles were missing. Photo evidence of an ScanEagle in Iran showed no U.S. military markings. It was also reported that Iran is producing a copied version of the ScanEagle and has put that UAV into military service.
Specifications
General characteristics
Crew
none on-board
Length
3.9 feet (1.19 meters)
Wingspan
10.2 feet (3.1 meters)
Loaded Weight
39.7 lbs (18 kilograms)
Powerplant
1 × 3W 2-stroke piston engine, 1.5 hp
Performance
Maximum speed
55-80 mph
Endurance
20 + hours
Service ceiling
16,000 feet above ground level (4,876 meters)

Avionics
High resolution, day/night camera and thermal imager

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The Northrop Grumman RQ-4 Global Hawk


The Northrop Grumman (formerly Ryan Aeronautical) RQ-4 Global Hawk is an unmanned aerial vehicle (UAV) used by the United States Air Force and Navy and the German Air Force as a surveillance aircraft.
In role and operational design, the Global Hawk is similar to the Lockheed U-2, the venerable 1950s spy plane. It is a theater commander's asset to provide a broad overview and systematic target surveillance. For this purpose, the Global Hawk is able to provide high resolution synthetic aperture radar (SAR) – that can penetrate cloud-cover and sandstorms – and electro-optical/infrared (EO/IR) imagery at long range with long loiter times over target areas. It can survey as much as 40,000 square miles (103,600 square kilometers) of terrain a day.
It is used as a high-altitude platform for surveillance and security. Missions for the Global Hawk cover the spectrum of intelligence collection capability to support forces in worldwide military operations. According to the United States Air Force, the capabilities of the aircraft allow more precise targeting of weapons and better protection of forces through superior surveillance capabilities. The Global Hawk costs about US$35 million to procure each aircraft. With development costs included, the unit cost rises to US$218 million.
Design
The RQ-4 is powered by an Allison Rolls-Royce AE3007H turbofan engine with 7,050 lbf (31.4 kN) thrust, and carries a payload of 2,000 pounds (900 kilograms). The main fuselage is standard aluminum, semi-monocoque construction, while the wings are made of lightweight, high-strength composite materials.
Integrated system
The Global Hawk UAV system comprises an air vehicle segment consisting of air vehicles with sensor payloads, avionics, and data links; a ground segment consisting of a Launch and Recovery Element (LRE), and a Mission Control Element (MCE) with embedded ground communications equipment; a support element; and trained personnel.
The Integrated Sensor Suite (ISS) is provided by Raytheon and consists of a synthetic aperture radar (SAR), electro-optical (EO), and infrared (IR) sensors. Either the EO or the IR sensors can operate simultaneously with the SAR. Each of the sensors provides wide area search imagery and a high-resolution spot mode. The SAR has a ground moving target indicator (GMTI) mode, which can provide a text message providing the moving target's position and velocity. Both SAR and EO/IR imagery are processed on board the aircraft and transmitted to the MCE as individual frames. The MCE can mosaic these frames into images prior to further dissemination.
Navigation is via inertial navigation with integrated Global Positioning System updates. Global Hawk is intended to operate autonomously and "untethered" using a satellite data link (either Ku or UHF) for sending sensor data from the aircraft to the MCE. The common data link can also be used for direct down link of imagery when the UAV is operating within line-of-sight of users with compatible ground stations.
The ground segment consists of a Mission Control Element (MCE) and Launch and Recovery Element (LRE), provided by Raytheon. The MCE is used for mission planning, command and control, and image processing and dissemination; an LRE for controlling launch and recovery; and associated ground support equipment. (The LRE provides precision differential global positioning system corrections for navigational accuracy during takeoff and landings, while precision coded GPS supplemented with an inertial navigation system is used during mission execution.) By having separable elements in the ground segment, the MCE and the LRE can operate in geographically separate locations, and the MCE can be deployed with the supported command's primary exploitation site. Both ground segments are contained in military shelters with external antennas for line-of-sight and satellite communications with the air vehicles.
Sensor packages
The Global Hawk carries the Hughes Integrated Surveillance & Reconnaissance (HISAR) sensor system. HISAR is a lower-cost derivative of the ASARS-2 package that Hughes developed for the Lockheed U-2. HISAR is also fitted in the US Army's RC-7B Airborne Reconnaissance Low Multifunction (ARLM) manned surveillance aircraft, and is being sold on the international market. HISAR integrates a SAR-MTI system, along with an optical and an infrared imager. All three sensors are controlled and their outputs filtered by a common processor. The digital sensor data can be transmitted at up to 50 Mbit/s to a ground station in real time, either directly or through a communications satellite link.
The SAR-MTI system operates in the X-band and provides a number of operational modes:
The wide-area MTI mode can detect moving targets within a radius of 62 miles (100 kilometers).
The combined SAR-MTI strip mode provides 20 foot (6 meter) resolution over a swath 23 miles (37 kilometers) wide at ranges from 12.4 to 68 miles (20 to 110 kilometers).
The SAR spot mode can provide 6 foot (1.8 meter) resolution over 3.8 square miles (10 square kilometers), as well as provide a sea-surveillance function.
The visible and infrared imagers share the same gimballed sensor package, and use common optics, providing a telescopic close-up capability. It can be optionally fitted with an auxiliary SIGINT package. To improve survivability, the Global Hawk is fitted with a Raytheon developed AN/ALR-89 self-protection suite consisting of the AN/AVR-3 Laser Warning System, AN/APR-49 Radar Warning Receiver and a jamming system. An ALE-50 towed decoy also aids in the Global Hawk's deception of enemy air defenses.
In July 2006, the US Air Force began testing segments of the improved Global Hawk Block 30 upgrades in the Benefield Anechoic Facility at Edwards AFB. This version incorporates an extremely sensitive SIGINT processor known as the Advanced Signals Intelligence Payload.
In September 2006, testing began on a new specialty radar system, the Multi-Platform Radar Technology Insertion Program, or MP-RTIP, on board the Scaled Composites Proteus. Once validated, one Global Hawk will be modified to carry this radar set. Previously, the Air Force was considering a larger variant of the MP-RTIP (known as the Wide-Area Surveillance or WAS sensor) for the canceled E-10 MC2A testbed or E-8 Joint STARS aircraft.
In August 2010, Northrop announced that a new version, Block 40, was about to commence production; it would have a new sensor capabilities, including MP-RTIP radar, emphasising surveillance over reconnaissance. The Block 40 design also has a modified undercarriage.
Specifications

RQ-4A
General characteristics
Crew
0
Length
44 ft 5 in (13.54 m)
Wingspan
116 ft 2 in (35.41 m)
Height
15 ft 2 in (4.62 m)
Empty weight
8,490 lb (3,851 kg)
Gross weight
22,900 lb (10,387 kg)
Powerplant
1 × Allison Rolls-Royce AE3007H turbofan engine, 7,050 lbf (31.4 kN) thrust

Performance
Maximum speed
497.1 mph (800 km/h; 432 kn)
Cruise speed
404 mph (351 kn; 650 km/h)
Range
15,525 mi (13,491 nmi; 24,985 km)
Endurance
36 hours
Service ceiling
65,000 ft (19,812 m)

RQ-4B
General characteristics
Crew
0 onboard (3 remote: LRE pilot; MCE pilot and sensor operator)
Length
47.6 ft (14.5 m)
Wingspan
130.9 ft (39.9 m)
Height
15.3 ft (4.7 m)
Empty weight
14,950 lb (6,781 kg)
Gross weight
32,250 lb (14,628 kg)
Powerplant
1 × Allison Rolls-Royce F137-RR-100 turbofan engine, 7,600 lbf (34 kN) thrust

Performance
Cruise speed
357 mph (310 kn; 575 km/h)
Range
8,700 mi (7,560 nmi; 14,001 km)
Endurance
28 hours
Service ceiling
60,000 ft (18,288 m)

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Northrop Grumman MQ-4C Triton


The Northrop Grumman MQ-4C Triton is an unmanned aerial vehicle (UAV) under development for the United States Navy as a surveillance aircraft. Developed under the Broad Area Maritime Surveillance (BAMS) program, the system is intended to provide continuous maritime surveillance for the US Navy, and to complement the Boeing P-8 Poseidon, the Boeing 737-based Multimission Maritime Aircraft (MMA).
The system is expected to enter service around 2015. Around 40 UAVs will be based at various sites - including Hawaii; Diego Garcia; NAS Jacksonville, Florida; Kadena Air Base, Japan; NAS Point Mugu, California, and NAS Sigonella, Italy. The Air Force Times reported on September 14, 2012, that the system will also be stationed at Andersen Air Force Base, Guam.
Development
Contract competition
The competitors for the contract included:
Boeing, with an unmanned version of the Gulfstream G550 business jet. It was optionally manned and has "commonality with other Boeing-built naval aircraft."
Northrop Grumman, with a marinized RQ-4 Global Hawk. In order to begin testing the surveillance package early, Northrop Grumman contracted with Flight Test Associates of the Mojave Spaceport to modify a Grumman Gulfstream II as a flying testbed.
Lockheed Martin, with a General Atomics Mariner
On 22 April 2008, Northrop Grumman received the Broad Area Maritime Surveillance contract worth $1.16 billion. Lockheed Martin filed a formal protest with the U.S. Government Accountability Office (GAO) two weeks later. On August 11, 2008 the GAO ruled to uphold the Navy’s selection of Northrop Grumman. In September 2010, the BAMS aircraft was designated the MQ-4C.
Initial development
Official unveiling took place on June 14, 2012 at Palmdale, California. During the event, it was announced that the Navy had approved the name "Triton" for the aircraft. First flight is expected by the end of 2012, followed by test flights at Edwards AFB and NAS Patuxent River. Initial Operational Capability is planned for December 2015.
The US Navy plans a fleet of 68 MQ-4Cs and 117 Boeing P-8As to replace the aging P-3 Orion force.
Specifications
General characteristics:
Crew: Unmanned, 4 per ground station
Length: 47.6 ft in (14.5 m)
Wingspan: 130.9 ft in (39.9 m)
Height: 15.3 ft in (4.7 m)
Gross weight: 32,250 lb (14,628.4 kg)
Powerplant: 1 × Rolls-Royce AE 3007 turbofan, 6,495-8,917 lbf (28.9-39.7 kN)
Performance:
Maximum speed: 357 mph (575 km/h)
Endurance: 30 hours
Service ceiling: 60,000 ft (18,288 m)

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MQ-1 Predator


The General Atomics MQ-1 Predator is an unmanned aerial vehicle (UAV) used primarily by the United States Air Force (USAF) and Central Intelligence Agency (CIA). Initially conceived in the early 1990s for reconnaissance and forward observation roles, the Predator carries cameras and other sensors but has been modified and upgraded to carry and fire two AGM-114 Hellfire missiles or other munitions. The aircraft, in use since 1995, has seen combat over Afghanistan, Pakistan, Bosnia, Serbia, Iraq, Yemen, Libya, and Somalia.
The USAF describes the Predator as a "Tier II" MALE UAS (medium-altitude, long-endurance unmanned aircraft system). The UAS consists of four aircraft or "air vehicles" with sensors, a ground control station (GCS), and a primary satellite link communication suite. Powered by a Rotax engine and driven by a propeller, the air vehicle can fly up to 400 nautical miles (740 km) to a target, loiter overhead for 14 hours, then return to its base.
Following 2001, the RQ-1 Predator became the primary unmanned aircraft used for offensive operations by the USAF and the CIA in Afghanistan and the Pakistani tribal areas; it has also been deployed elsewhere. Because offensive uses of the Predator are classified, U.S. military officials have reported an appreciation for the intelligence and reconnaissance-gathering abilities of UAVs but declined to publicly discuss their offensive use.
Design
The Central Intelligence Agency (CIA) and the Pentagon began experimenting with reconnaissance drones in the early 1980s. The CIA preferred small, lightweight, unobtrusive drones, in contrast to the United States Air Force (USAF). In the early 1990s, the CIA became interested in the "Amber", a drone developed by Leading Systems, Inc. The company's owner, Abraham Karem, was the former chief designer for the Israeli Air Force, and had immigrated to the U.S. in the late 1970s. Karem's company had since gone bankrupt and been bought up by a U.S. defense contractor, from whom the CIA secretly bought five drones (now called the "GNAT"). Karem agreed to produce a quiet engine for the vehicle, which had until then sounded like "a lawnmower in the sky". The new development became known as the "Predator".
General Atomics Aeronautical Systems (GA) was awarded a contract to develop the Predator in January 1994, and the initial Advanced Concept Technology Demonstration (ACTD) phase lasted from January 1994 to June 1996. The aircraft itself was a derivative of the GA Gnat 750. During the ACTD phase, three systems were purchased from GA, comprising twelve aircraft and three ground control stations.
From April through May 1995, the Predator ACTD aircraft were flown as a part of the Roving Sands 1995 exercises in the U.S. The exercise operations were successful, and this led to the decision to deploy the system to the Balkans later in the summer of 1995.
During the ACTD, Predators were operated by a combined Army/Navy team managed by the Navy's Joint Program Office for Unmanned Aerial Vehicles (JPO-UAV) and first deployed to Gjader, Albania, for operations in the Former Yugoslavia in Spring 1995.
By the start of the United States Afghan campaign in 2001, the USAF had acquired 60 Predators, and said it had lost 20 of them in action. Few if any of the losses were from enemy action, the worst problem apparently being foul weather, particularly icy conditions. Some critics within the Pentagon saw the high loss rate as a sign of poor operational procedures. In response to the losses caused by cold weather flight conditions, a few of the later Predators obtained by the USAF were fitted with de-icing systems, along with an uprated turbocharged engine and improved avionics. This improved "Block 1" version was referred to as the "RQ-1B", or the "MQ-1B" if it carried munitions; the corresponding air vehicle designation was "RQ-1L" or "MQ-1L".
The Predator system was initially designated the RQ-1 Predator. The "R" is the United States Department of Defense designation for reconnaissance and the "Q" refers to an unmanned aircraft system. The "1" describes it as being the first of a series of aircraft systems built for unmanned reconnaissance. Pre-production systems were designated as RQ-1A, while the RQ-1B (not to be confused with the RQ-1 Predator B, which became the MQ-9 Reaper) denotes the baseline production configuration. These are designations of the system as a unit. The actual aircraft themselves were designated RQ-1K for pre-production models, and RQ-1L for production models. In 2002, the USAF officially changed the designation to MQ-1 ("M" for multi-role) to reflect its growing use as an armed aircraft.
Command and sensor systems
During the campaign in the former Yugoslavia, a Predator's pilot would sit with several payload specialists in a van near the runway of the drone's operating base. Direct radio signals controlled the drone's takeoff and initial ascent. Then communications shifted to military satellite networks linked to the pilot's van. Pilots experienced a delay of several seconds between moving their joysticks and the drone's response. But by 2000 improvements in communications systems (perhaps by use of the USAF's JSTARS system) made it possible, at least in theory, to fly the drone remotely from great distances. It was no longer necessary to use close-up radio signals during the Predator's takeoff and ascent. The entire flight could be controlled by satellite from any command center with the right equipment. The CIA proposed to attempt over Afghanistan the first fully remote Predator flight operations, piloted from the agency's headquarters at Langley.
The Predator air vehicle and sensors are controlled from the ground station via a C-band line-of-sight data link or a Ku-band satellite data link for beyond-line-of-sight operations. During flight operations the crew in the ground control station is a pilot and two sensor operators. The aircraft is equipped with the AN/AAS-52 Multi-spectral Targeting System, a color nose camera (generally used by the pilot for flight control), a variable aperture day-TV camera, and a variable aperture infrared camera (for low light/night). Previously, Predators were equipped with a synthetic aperture radar for looking through smoke, clouds or haze, but lack of use validated its removal to reduce weight and conserve fuel. The cameras produce full motion video and the synthetic aperture radar produced still frame radar images. There is sufficient bandwidth on the datalink for two video sources to be used at one time, but only one video source from the sensor ball can be used at any time due to design limitations. Either the daylight variable aperture or the infrared electro-optical sensor may be operated simultaneously with the synthetic aperture radar, if equipped. All later Predators are equipped with a laser designator that allows the pilot to identify targets for other aircraft and even provide the laser-guidance for manned aircraft. This laser is also the designator for the AGM-114 Hellfire that are carried on the MQ-1.
Deployment methodology
Each Predator air vehicle can be disassembled into six main components and loaded into a container nicknamed "the coffin." This enables all system components and support equipment to be rapidly deployed worldwide. The largest component is the ground control station and it is designed to roll into a C-130 Hercules. The Predator primary satellite link consists of a 6.1 meter (20 ft) satellite dish and associated support equipment. The satellite link provides communications between the ground station and the aircraft when it is beyond line-of-sight and is a link to networks that disseminate secondary intelligence. The RQ-1A system needs 1,500 by 40 meters (5,000 by 125 ft) of hard surface runway with clear line-of-sight to each end from the ground control station to the air vehicles. Initially, all components needed to be located on the same airfield.
Currently, the U.S. Air Force uses a concept called "Remote-Split Operations" where the satellite datalink is located in a different location and is connected to the GCS through fiber optic cabling. This allows Predators to be launched and recovered by a small "Launch and Recovery Element" and then handed off to a "Mission Control Element" for the rest of the flight. This allows a smaller number of troops to be deployed to a forward location, and consolidates control of the different flights in one location.
The improvements in the MQ-1B production version include an ARC-210 radio, an APX-100 IFF/SIF with mode 4, a glycol-weeping "wet wings" ice mitigation system, up-graded turbo-charged engine, fuel injection, longer wings, dual alternators as well as other improvements.
On May 18, 2006, the Federal Aviation Administration (FAA) issued a certificate of authorization which will allow the M/RQ-1 and M/RQ-9 aircraft to be used within U.S. civilian airspace to search for survivors of disasters. Requests had been made in 2005 for the aircraft to be used in search and rescue operations following Hurricane Katrina, but because there was no FAA authorization in place at the time, the assets were not used. The Predator's infrared camera with digitally-enhanced zoom has the capability of identifying the heat signature of a human body from an altitude of 3 km (10,000 ft), making the aircraft an ideal search and rescue tool.
The longest declassified Predator flight to date lasted for 40 hours, 5 minutes. The total flight time has reached 1 million hours as of April 2010.
Armed version development
The USAF handed the Predator over to the service's Big Safari office after the Kosovo campaign in order to accelerate its testing in a strike role, fitted with reinforced wings and stores pylons to carry munitions, as well as a laser designator. This effort led to a series of tests, on February 21, 2001, in which the Predator fired three Hellfire anti-armor missiles, scoring hits on a stationary tank with all three missiles. The scheme was put into service, with the armed Predators given the new designation of MQ-1A. Given that a Predator is very unobtrusive and the Hellfire is supersonic, such a combination gives little warning of attack.
In the winter of 2000–2001, after seeing the results of Predator reconnaissance in Afghanistan, Cofer Black, head of the CIA's Counterterrorist Center (CTC), became a "vocal advocate" of arming the Predator with missiles to target Osama bin Laden in the country. He also believed that CIA pressure and practical interest was causing the USAF's armed Predator program to be significantly accelerated. Black, and "Richard", who was in charge of the CTC's Bin Laden Issue Station, continued to press during 2001 for a Predator armed with Hellfire missiles.
Further weapons tests occurred between May 22 and June 7, 2001, with mixed results. While missile accuracy was excellent, there were some problems with missile fuzing" In the first week of June, in the Nevada Desert, a Hellfire missile was successfully launched on a replica of bin Laden's Afghanistan Tarnak residence. A missile launched from a Predator exploded inside one of the replica's rooms; it was concluded that any people in the room would have been killed. However, the armed Predator did not go into action before the September 11 attacks.
The USAF has also investigated using the Predator to drop battlefield ground sensors and to carry and deploy the "Finder" mini-UAV.

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