TAI Aksungur

The TAI Aksungur is an unmanned aerial vehicle (UAV) in development by Turkish Aerospace Industries (TAI) for the Turkish Armed Forces. Using existing technology from the TAI Anka series of drones, it is the manufacturer's largest drone  with payload capacity for mission-specific equipment. It is intended to be used for long-term surveillance, signals intelligence, maritime patrol missions, or as an unmanned combat aerial vehicle. TAI planned to integrate weapon packages and put the Aksungur into production in early 2020.



TAI Aksungur




Development

Aksungur, Turkish for gyrfalcon,[5] is classified as a medium-altitude long-endurance (MALE) unmanned aerial vehicle (UAV). It is designed and manufactured by Turkish Aerospace Industries (TAI) for tactical surveillance and reconnaissance missions of the Turkish Armed Forces.  The Aksungur has twin turbocharged engines with a twin boom configuration. 


Developing the UAV took 18 months. The airframe, wing and landing gear are new designs, while control systems are from the existing TAI Anka family of drones. A new turbodiesel engine is also in development for the programme, with initial flight tests of the airframe using an existing engine.  Two prototypes were manufactured for testing purposes. Its maiden flight, displaying automatic takeoff and landing capabilities, took place on 20 March 2019, and lasted four hours and twenty minutes.  Reportedly, a second test flight of three hours was performed on 3 April the same year. It was introduced at the 2019 International Defence Industry Fair (IDEF) in Istanbul, Turkey, on 30 April.  CNN Türk reported ongoing flight tests in July 2019,  with the manufacturer anticipating a total of 50 to 60 tests by the end of the year.  The UAV is planned to go into series production by the first quarter of 2020.

TAI Aksungur

Design

The aircraft is 12 m (39 ft) long and 3 m (9.8 ft) high when resting on its landing gear. The high-mounted wings have a slight dihedral angle and a wingspan of 24 m (79 ft).[1] The wings end with small winglets. The centralized fuselage is under the wings and houses avionics, camera and sensors systems, with a chin-mounted camera blister. Fuel is stored in the fuselage[11] and wings. A turbocharged engine is mounted under each wing, with the engine nacelles each extending backward into a tail boom. These tail booms terminate in vertical stabilizers, with a horizontal tailplane joining them. The tricycle landing gear retracts into the engine nacelles and the nose of the aircraft while in flight. 


The aircraft is powered by two forward-mounted PD-170 dual-turbocharged diesel engines developed by Tusaş Engine Industries (TEI), equipped with three-bladed propellers in a tractor (puller) configuration.[1] According to the manufacturer, these enable the Aksungur to cruise at a maximum speed of 180 km/h (110 mph) and carry a maximum payload of 750 kg (1,650 lb)  to an altitude of 25,000 ft (7,600 m), or ascend to 35,000 ft (11,000 m) with a 150 kg (330 lb) payload. The aircraft's designed maximum payload is 375% greater than that of its predecessor;[4] its maximum takeoff weight is 3,300 kg (7,300 lb). It is rated to stay aloft 12 hours as an attack aircraft or maritime patrol aircraft and 24 hours during signals intelligence missions. 


Remote control of the UAV is performed by DO-178B compatible software on DO-254 compatible ground control station and hardware using double backed-up encrypted digital data link. Optional beyond-visual-range operation flexibility is available via communications satellite. 


TAI expects to integrate weapon systems typical of F-4 and F-16 fighter aircraft[8] onto Aksungur in the last quarter of 2019.  Three hardpoints are situated under each wing for attaching external payloads, such as munitions or sonar buoys. These hardpoints are rated for loads of 150, 300 and 500 kg (330, 660 and 1,100 lb). Proposed armaments include TEBER-81 (laser-guided bomb Mk-81), TEBER-82 (laser-guided bomb Mk-82), LUMTAS, MAM-L, Roketsan Cirit, MAM-C, HGK-3 (precision-guided munition), KGK (82) (winged guided kit), and miniature bomb. 


TAI Aksungur

Specifications

Data from Tusaş, Jane's Information Group and Military Factory

General characteristics

  • Capacity: 1,653 lb (750 kg) payload
  • Length: 12 m (39 ft 4 in)
  • Wingspan: 24 m (78 ft 9 in)
  • Height: 3 m (9 ft 10 in)
  • Empty weight: 1,800 kg (3,968 lb)
  • Max takeoff weight: 3,300 kg (7,275 lb)
  • Powerplant: 2 × TEI PD170 4-cylinder liquid-cooled turbo-charged horizontally-opposed piston engine, 130–160 kW (170–220 hp) each
  • Propellers: 3-bladed constant-speed pusher propeller

Performance

  • Cruise speed: 250 km/h (160 mph, 130 kn)
  • Range: 6,500 km (4,000 mi, 3,500 nmi)
  • Endurance: 49 hours
  • Service ceiling: 12,192 m (40,000 ft)

Armament

  • Hardpoints: 6 with provisions to carry combinations of:
    • Missiles:
    • Rockets
      • Possibly ROKETSAN DSH(Anti Submarine Warfare Rocket) and torpedoes for maritime patrol duties.
    • Bombs:

 sources: wikipediadefenceturkey, janes, militaryfactory

 

General Atomics MQ-9 Reaper

General Atomics MQ-9 Reaper


The General Atomics MQ-9 Reaper (sometimes called Predator B) is an unmanned aerial vehicle (UAV) capable of remotely controlled or autonomous flight operations developed by General Atomics Aeronautical Systems (GA-ASI) primarily for the United States Air Force (USAF). The MQ-9 and other UAVs are referred to as Remotely Piloted Vehicles/Aircraft (RPV/RPA) by the USAF to indicate their human ground controllers. 

The MQ-9 is the first hunter-killer UAV designed for long-endurance, high-altitude surveillance. In 2006, the then–Chief of Staff of the United States Air Force General T. Michael Moseley said: "We've moved from using UAVs primarily in intelligence, surveillance, and reconnaissance roles before Operation Iraqi Freedom, to a true hunter-killer role with the Reaper." 

The MQ-9 is a larger, heavier, and more capable aircraft than the earlier General Atomics MQ-1 Predator; it can be controlled by the same ground systems used to control MQ-1s. The Reaper has a 950-shaft-horsepower (712 kW) turboprop engine (compared to the Predator's 115 hp (86 kW) piston engine). The greater power allows the Reaper to carry 15 times more ordnance payload and cruise at about three times the speed of the MQ-1. The aircraft is monitored and controlled by aircrew in the Ground Control Station (GCS), including weapons employment. 

In 2008, the New York Air National Guard 174th Attack Wing began the transition from F-16 piloted fighters to MQ-9A Reapers, becoming the first fighter unit to convert entirely to unmanned combat aerial vehicle (UCAV) use. In March 2011, the U.S. Air Force was training more pilots for advanced unmanned aerial vehicles than for any other single weapons system.  The Reaper is also used by the U.S. Customs and Border Protection, and the militaries of several other countries.

The USAF operated 195 MQ-9 Reapers as of September 2016, and plans to keep the MQ-9 in service into the 2030s.


Development

Origins

The General Atomics "Predator B-001", a proof-of-concept aircraft, first flew on 2 February 2001. Abraham Karem is the designer of the Predator.[9] The B-001 was powered by an AlliedSignal Garrett TPE331-10T turboprop engine with 950 shaft horsepower (710 kW). It had an airframe that was based on the standard Predator airframe, except with an enlarged fuselage and wings lengthened from 48 feet (15 m) to 66 feet (20 m). The B-001 had a speed of 220 knots (410 km/h; 250 mph) and could carry a payload of 750 pounds (340 kg) to an altitude of 50,000 feet (15,000 m) with an endurance of 30 hours. 


The company refined the design, taking it in two separate directions. The first was a jet-powered version; "Predator B-002" was fitted with a Williams FJ44-2A turbofan engine with 10.2 kilonewtons (2,300 lbf; 1,040 kgf) thrust. It had payload capacity of 475 pounds (215 kg), a ceiling of 60,000 feet (18 km) and endurance of 12 hours. The USAF ordered two airframes for evaluation, delivered in 2007.[11] The first two airframes delivered with prototypes B-001 and B-002 (now in the USAF museum at Wright-Patterson AFB). B-002 was originally equipped with the FJ-44 engine but it was removed and a TPE-331-10T was installed so that the USAF could take delivery of two aircraft in the same configuration.


The second direction the design took was the "Predator B-003", referred to by GA as the "Altair", which has a new airframe with an 84-foot (26 m) wingspan and a takeoff weight of approximately 7,000 pounds (3,200 kg). Like the Predator B-001, it is powered by a TPE-331-10YGD turboprop. This variant has a payload capacity of 3,000 pounds (1,400 kg), a maximum ceiling of 52,000 feet (16 km), and an endurance of 36 hours.


In October 2001, the USAF signed a contract for an initial pair of Predator Bs (001 and 002) for evaluation. Designated YMQ-9s due to their prototype role, they were delivered in 2002. The USAF referred to it as "Predator B" until it was renamed "Reaper". The USAF aimed for the Predator B to provide an improved "deadly persistence" capability, flying over a combat area night-and-day waiting for a target to present itself, complementing piloted attack aircraft, typically used to drop larger quantities of ordnance on a target, while a cheaper RPV can operate almost continuously using ground controllers working in shifts, but carrying less ordnance.

General Atomics MQ-9 Reaper


Operation

MQ-9 Reaper crews (Pilots, Sensor Operators and Mission Intelligence Coordinators), stationed at bases such as Creech Air Force Base, near Las Vegas, Nevada, can hunt for targets and observe terrain using multiple sensors, including a thermographic camera. One claim was that the on-board camera is able to read a license plate from two miles (3.2 km) away.[14] An operator's command takes 1.2 seconds to reach the drone via a satellite link. The MQ-9 is fitted with six stores pylons; the inner stores pylons can carry a maximum of 1,500 pounds (680 kg) each and allow carriage of external fuel tanks. The mid-wing stores pylons can carry a maximum of 600 pounds (270 kg) each, while the outer stores pylons can carry a maximum of 200 pounds (91 kg) each. An MQ-9 with two 1,000 pounds (450 kg) external fuel tanks and 1,000 pounds (450 kg) of munitions has an endurance of 42 hours.[13] The Reaper has an endurance of 14 hours when fully loaded with munitions.[4] The MQ-9 carries a variety of weapons including the GBU-12 Paveway II laser-guided bomb, the AGM-114 Hellfire II air-to-ground missiles, the AIM-9 Sidewinder, and the GBU-38 Joint Direct Attack Munition (JDAM). Tests are underway to allow for the addition of the AIM-92 Stinger air-to-air missile.[citation needed]


By October 2007, the USAF owned nine Reapers, and by December 2010 had 57 with plans to buy another 272, for a total of 329 Reapers.[16] Critics have stated that the USAF's insistence on qualified pilots flying RPVs is a bottleneck to expanding deployment. USAF Major General William Rew stated on 5 August 2008, "For the way we fly them right now"—fully integrated into air operations and often flying missions alongside manned aircraft—"we want pilots to fly them." This reportedly has exacerbated losses of USAF aircraft in comparison with US Army operations.  In March 2011, U.S. Department of Defense Secretary Robert Gates stated that, while manned aircraft are needed, the USAF must recognize "the enormous strategic and cultural implications of the vast expansion in remotely piloted vehicles..." and stated that as the service buys manned fighters and bombers, it must give equal weight to unmanned drones and "the service's important role in the cyber and space domains."


In 2013, the Air Force Special Operations Command (AFSOC) sought the ability to pack up an MQ-9 in less than eight hours, fly it anywhere in the world aboard a C-17 Globemaster III, and then have it ready to fly in another eight hours to support special operations teams at places with no infrastructure. MQ-1 and MQ-9 drones must fly aboard cargo aircraft to travel long distances as they lack the refueling technology or speed to travel themselves; the C-17 is large enough to carry the aircraft and support systems and can land on short runways. Pilots traveling with the Reaper will use the ground control station to launch and land the aircraft, while most of the flying will be done by US-based pilots. 


Testbed and upgrades

In November 2012, Raytheon completed ground verification tests for the ADM-160 MALD and MALD-J for integration onto the Reaper for an unmanned suppression of enemy air defenses capability. On 12 April 2013, a company-owned MQ-9 equipped with a jamming pod and digital receiver/exciter successfully demonstrated its electronic warfare capability at Marine Corps Air Station (MCAS) Yuma, performing its mission in coordination with over 20 participating aircraft. A second electronic warfare test, fitted with the Northrop Grumman Pandora EW System, was conducted on 22 October 2013 with other unmanned aircraft and Northrop Grumman EA-6B Prowlers, showing effectiveness in a multi-node approach against a more capable IADS. 


In 2011, the U.S. Missile Defense Agency (MDA) reported its interest in using the Reaper and its MTS-B sensor to provide firing quality data for early interception of ballistic missile launches. The MDA is exploring concepts to use the UAV's EO/IR sensor to achieve "launch-on-remote" capabilities with missile interceptors before detection by Aegis radars. At least two aircraft would be needed to triangulate a target to provide high-fidelity data. The MTS-B includes short and mid-wave IR bands, optimal for tracking launch and rocket burn. In 2013, the MDA terminated plans to build a follow-on to the two orbiting Space Tracking and Surveillance System (STSS) satellites due to near-term costs, opting to continue testing the Reaper for ballistic missile target discrimination. The MDA planned to test the improved MTS-C sensor, which adds a long-wave IR detector optimized for tracking cold bodies such as missiles and warheads after booster burnout, or plumes and exhaust. The goal is to use data from multiple high-flying UAVs to provide an off-board cue to launch an SM-3 missile from an Aegis ship. Two Reapers demonstrated their ability to track ballistic missiles using their MTS-B EO/IR turret during a test in late June 2016. 


In June 2015, a study by the USAF's Scientific Advisory Board identified several improvements for operating the Reaper in contested airspace; adding readily available sensors, weapons, and threat detection and countermeasures could increase situational awareness and enable riskier deployments. Suggestions included a radar warning receiver (RWR) to know when it's being targeted, air-to-air and miniature air-to-ground weapons, manned-unmanned teaming, multi-UAV control, automatic take-offs and landings, and precision navigation and timing systems to fly in GPS-denied areas. Another idea was redesigned ground control stations with user-friendly video game-like controllers and touchscreen maps to access data without overwhelming operators. 


In October 2015, Air Force deputy chief of staff for ISR Robert Otto suggested redesigning the MQ-9's GCS to be operated by one person for most missions rather than two (to fly and work the sensors) to simplify operations and reduce manpower requirements by hundreds of sensor operators. Introducing an auto-land capability would also reduce the Reaper's manpower requirements to staff launch and recovery teams.  Automatic take-off and landing capabilities are already present in the RQ-4 Global Hawk and MQ-1C Gray Eagle, and are planned to be provided to the MQ-9 in 2017. The Air Force requires the manually loaded Reaper to operate from a runway at least 5,000 ft (1.5 km) long, but automated take-offs and landings would enable it to operate from a 3,000 ft (0.91 km) runway. 


In April 2017, an MQ-9 Block 5 flew with a Raytheon ALR-69A RWR in its payload pod to demonstrate the aircraft's ability to conduct missions in the proximity of threat radars and air defenses, the first time this capability was demonstrated on a remotely piloted aircraft. In September 2020, a Reaper was flown carrying two Hellfire missiles on each of the stations previously reserved for 500 lb bombs or fuel tanks. A software upgrade doubled the aircraft's capacity to eight missiles. 

General Atomics MQ-9 Reaper


Design

A typical MQ-9 system consists of multiple aircraft, ground control station, communications equipment, maintenance spares, and personnel. A military flight crew includes a pilot, sensor operator, and Mission Intelligence Coordinator.  The aircraft is powered by a 950 horsepower (710 kW) turboprop, with a maximum speed of about 260 knots (480 km/h; 300 mph) and a cruising speed of 150–170 knots (170–200 mph; 280–310 km/h). With a 66 ft (20 m) wingspan, and a maximum payload of 3,800 lb (1,700 kg), the MQ-9 can be armed with a variety of weaponry, including Hellfire missiles and 500-lb laser-guided bomb units.[34] Endurance is 30 hours when conducting ISR missions, which decreases to 23 hours if it is carrying a full weapons load.  The Reaper has a range of 1,000 nmi (1,150 mi; 1,850 km)[dubious – discuss] and an operational altitude of 50,000 ft (15,000 m), which makes it especially useful for long-term loitering operations, both for surveillance and support of ground troops.

The Predator and Reaper were designed for military operations and not intended to operate among crowded airline traffic. The aircraft typically lack systems capable of complying with FAA See-And-Avoid regulations. On 18 May 2006, the Federal Aviation Administration (FAA) issued a certificate of authorization allowing MQ-1 and MQ-9 UAVs to fly in U.S. civil airspace to search for survivors of disasters. In 2005, requests were made for MQ-9s to be used in search and rescue operations following Hurricane Katrina but, as there was no FAA authorization in place at the time, it was not used. 


An MQ-9 can adopt various mission kits and combinations of weapons and sensors payloads to meet combat requirements. Its Raytheon AN/AAS-52[citation needed] multi-spectral targeting sensor suite includes a color/monochrome daylight TV, infrared, and image-intensified TV with laser rangefinder/laser designator to designate targets for laser guided munitions.[citation needed] The aircraft is also equipped with the Lynx Multi-mode Radar that contains synthetic aperture radar (SAR) that can operate in both spotlight and strip modes, and ground moving target indication (GMTI) with Dismount Moving Target Indicator (DMTI) and Maritime Wide-Area Search (MWAS) capabilities.  The Reaper was used as a test bed for Gorgon Stare, a wide-area surveillance sensor system.  Increment 1 of the system was first fielded in March 2011 on the Reaper and could cover an area of 16 km2 (6.2 sq mi); increment 2, incorporating ARGUS-IS and expanding the coverage area to 100 km2 (39 sq mi), achieved initial operating capability (IOC) in early 2014. The system has 368 cameras capable of capturing five million pixels each to create an image of about 1.8 billion pixels; video is collected at 12 frames per second, producing several terabytes of data per minute. 


In January 2012, General Atomics released a new trailing arm design for the Reaper's main landing gear; benefits include an over 30 percent increase in landing weight capacity, a 12 percent increase in gross takeoff weight (from 10,500 pounds (4,800 kg) to 11,700 pounds (5,300 kg)), a maintenance-free shock absorber (eliminating the need for nitrogen pressurization), a fully rejected takeoff brake system, and provisions for automatic takeoff and landing capability and Anti-lock Brake System (ABS) field upgrades.  In April 2012, General Atomics announced possible upgrades to USAF Reapers, including two extra 100 US gallons (380 l) fuel pods under the wings to increase endurance to 37 hours. The wingspan can also be increased to 88 feet (27 m), increasing endurance to 42 hours. The USAF has bought 38 Reaper Extended Range (ER) versions, carrying external fuel tanks (which don't affect weapon capacity), the heavy-weight landing gear, a four-bladed propeller, a new fuel management system which ensures fuel and thermal balance among external tank, wing, and fuselage fuel sources, and an alcohol-water injection (AWI) system to shorten required runway takeoff length; these features increase endurance from 27 to 33–35 hours, while the company is still pitching the lengthened wing option. The Reaper ER first flew operationally in August 2015. The aircraft also has the sensor ball replaced with a high-definition camera, better communications so ground controllers can see the higher quality video, software to enable automatic detection of threats and tracking of 12 moving targets at once, and the ability to "super ripple" fire missiles within 0.32 seconds of each other.


On 25 February 2016, General Atomics announced a successful test flight of the new Predator-B/ER version. This new version has had the wingspan extended to 79 feet, increasing its endurance to 40 hours. Other improvements include "short-field takeoff and landing performance and spoilers on the wings which enable precision automatic landings. The wings also have provisions for leading-edge de-ice and integrated low- and high-band RF antennas."

MQ-9 Reaper / Predator B
MQ-9 Reaper UAV (cropped).jpg
U.S. Air Force MQ-9A Reaper
RoleUnmanned combat aerial vehicle
National originUnited States
ManufacturerGeneral Atomics Aeronautical Systems
First flight2 February 2001; 19 years ago
Introduction1 May 2007
StatusIn service
Primary usersUnited States Air Force
  • U.S. Customs and Border Protection
  • Royal Air Force
  • Italian Air Force
Number built195+ as of 2016
Developed fromGeneral Atomics MQ-1 Predator
Developed intoGeneral Atomics Avenger


 source : wikipedia

Unmanned aerial vehicle (UAV)

Unmanned aerial vehicle (UAV)


An unmanned aerial vehicle (UAV) (or uncrewed aerial vehicle,[  commonly known as a drone) is an aircraft without a human pilot on board. UAVs are a component of an unmanned aircraft system (UAS); which include a UAV, a ground-based controller, and a system of communications between the two.  The flight of UAVs may operate with various degrees of autonomy: either under remote control by a human operator or autonomously by onboard computers referred to as an autopilot.

Compared to crewed aircraft, UAVs were originally used for missions too "dull, dirty or dangerous"  for humans. While drones originated mostly in military applications, their use is rapidly finding many more applications including aerial photography, product deliveries, agriculture, policing and surveillance, infrastructure inspections, science,  smuggling, and drone racing.


Terminology

Multiple terms are used for unmanned aerial vehicles, generally referring to the same concept.

The term drone, more widely used by the public, was coined in reference to the early remotely-flown target aircraft used for practice firing of a battleship's guns, and the term was first used with the 1920s Fairey Queen and 1930's de Havilland Queen Bee target aircraft. These two were followed in service by the similarly named Airspeed Queen Wasp and Miles Queen Martinet, before ultimate replacement by the GAF Jindivik.

The term unmanned aircraft system (UAS) was adopted by the United States Department of Defense (DoD) and the United States Federal Aviation Administration in 2005 according to their Unmanned Aircraft System Roadmap 2005–2030. The International Civil Aviation Organization (ICAO) and the British Civil Aviation Authority adopted this term, also used in the European Union's Single-European-Sky (SES) Air-Traffic-Management (ATM) Research (SESAR Joint Undertaking) roadmap for 2020.This term emphasizes the importance of elements other than the aircraft. It includes elements such as ground control stations, data links and other support equipment. A similar term is an unmanned-aircraft vehicle system (UAVS), remotely piloted aerial vehicle (RPAV), remotely piloted aircraft system (RPAS). Many similar terms are in use.

Unmanned aerial vehicle (UAV)


A UAV is defined as a "powered, aerial vehicle that does not carry a human operator, uses aerodynamic forces to provide vehicle lift, can fly autonomously or be piloted remotely, can be expendable or recoverable, and can carry a lethal or nonlethal payload". Therefore, missiles are not considered UAVs because the vehicle itself is a weapon that is not reused, though it is also uncrewed and in some cases remotely guided. That being said, UAV is a term that is commonly applied to military use cases.[16]

The terms autonomous drone and UAV are often wrongfully used interchangeably. This could stem from the fact that many UAVs are automated, i.e. they carry out automated missions but still rely on human operators. However, an autonomous drone is a "UAV that can operate without any human intervention". In other words, autonomous drones take off, carry out missions, and land completely autonomously. Thus, an autonomous drone is a type of UAV but a UAV is not necessarily an autonomous drone.

As autonomous drones are not piloted by humans, a ground control system, or communications management software, plays a major role in their operations, and thus they are also considered part of a UAS. In addition to the software, autonomous drones also employ a host of advanced technologies that allow them to carry out their missions without human intervention, such as cloud computing, computer vision, artificial intelligence, machine learning, deep learning, and thermal sensors.

In recent years, autonomous drones have begun to transform various commercial industries as they can fly beyond visual line of sight (BVLOS) while maximizing production, reducing costs and risks, ensuring site safety, security and regulatory compliance, and protecting the human workforce in times of a pandemic. They can also be used for consumer-related missions like package delivery, as demonstrated by Amazon Prime Air, and critical deliveries of health supplies.

A Drone-in-a-Box (DIB) is an autonomous drone that deploys to carry out a pre-programmed list of missions from and returns to a self-contained landing box that also functions as the drone's charging base.

Under new regulations which came into effect 1 June 2019, the term RPAS (Remotely Piloted Aircraft System) has been adopted by the Canadian Government to mean "a set of configurable elements consisting of a remotely piloted aircraft, its control station, the command and control links and any other system elements required during flight operation".

The relation of UAVs to remote controlled model aircraft is unclear.[citation needed] UAVs may or may not include model aircraft. Some jurisdictions base their definition on size or weight; however, the US Federal Aviation Administration defines any uncrewed flying craft as a UAV regardless of size. For recreational uses, a drone (as opposed to a UAV) is a model aircraft that has first-person video, autonomous capabilities, or both.


Sourec: wikipedia

Military personnel

Military personnel


Military personnel are members of the state's armed forces. Their roles, pay, and obligations differ according to their military branch (army, navy, marines, air force, space force, and sometimes coast guard), rank (officer, non-commissioned officer, or enlisted recruit), and their military task when deployed on operations and on exercise.


Overview

Those who serve in a typical large land force are soldiers, making up an army. Those who serve in seagoing forces are seamen or sailors, and their branch is a navy or coast guard. Marines serve in a marine corps. In the 20th century, the development of powered flight aircraft prompted the development of air forces, serviced by airmen and women. In the 21st century, the fervent return to extraterrestrial activities spawned the first space force, peopled by guardians, aided by rudimentary automated systems.


Designated leaders of military personnel are officers. These include commissioned officers, warrant officers and non-commissioned officers (NCOs). For naval forces, non-commissioned officers are referred to as petty officers.


Organizations other than state armed forces include military personnel, such as paramilitary organizations and non-state armed groups.


Demographics

Most personnel at the start of their military career are young adults. For example, in 2013 the average age of a United States Army soldier beginning initial training was 20.7 years. Historically, the use of children under the age of 18 for military purposes has been widespread – see Children in the military – but has been in decline in the 21st century. According to Child Soldiers International, as of 2017 approximately two-thirds of states worldwide had committed to restrict military recruitment to adults, while 50 states were still recruiting personnel aged 16 or 17, including most of the world's major military powers.


Most personnel are male. The proportion of female personnel varies internationally; for example, it is approximately 3% in India, 10% in the UK, 13% in Sweden, 16% in the US, and 27% in South Africa. Many state armed forces that recruit women bar them from ground close combat roles (roles that would require them to kill at close quarters).Compared with male personnel and female civilians, female personnel face substantially higher risks of sexual harassment and sexual violence, according to British, Canadian, and US research.


Personnel who join as officers tend to be upwardly-mobile young adults from age 18.Most enlisted personnel have a childhood background of relative socio-economic deprivation. For example, after the US suspended conscription in 1973, 'the military disproportionately attracted African American men, men from lower-status socioeconomic backgrounds, men who had been in nonacademic high school programs, and men whose high school grades tended to be low'. However, a 2020 study suggests that U.S. Armed Forces personnel's socio-economic status are at parity or slightly higher than the civilian population and that the most disadvantaged socio-economic groups are less likely to meet the requirements of the modern U.S. military. As an indication of the socio-economic background of British Army personnel, in 2015 three-quarters of its youngest recruits had the literacy skills normally expected of an 11-year-old or younger, and 7% had a reading age of 5–7.

Military personnel


Recruitment

Military personnel may be conscripted (recruited by compulsion under the law) or recruited by attracting civilians to join the armed forces.


Initial training

Military personnel must be prepared to perform tasks that in civilian life would be highly unusual or absent. In particular, they must be capable of injuring and killing other people, and of facing mortal danger without fleeing. This is achieved in initial training, a physically and psychologically intensive process which resocializes recruits for the unique nature of military demands.


According to an expert in military training methods, Lt Col. Dave Grossman, initial training uses four conditioning techniques: role modeling, classical conditioning, operant conditioning, and brutalization. For example, throughout initial training:

  • Individuality is suppressed (e.g. by shaving the head of new recruits, issuing uniforms, denying privacy, and prohibiting the use of first names);
  • Daily routine is tightly controlled (e.g. recruits must make their beds, polish boots, and stack their clothes in a certain way, and mistakes are punished);
  • Continuous stressors deplete psychological resistance to the demands of their instructors (e.g. depriving recruits of sleep, food, or shelter, shouting insults and giving orders intended to humiliate); and
  • Frequent punishments serve to condition group conformity and discourage poor performance.
  • The disciplined drill instructor is presented as a role model of the ideal soldier.

In conditions of continuous physical and psychological stress, the trainee group normally forms a bond of mutual loyalty, commonly experienced as an emotional commitment. It has been called a "we-feeling", and helps to commit recruits to their military organisation.

Throughout their initial training, recruits are repeatedly instructed to stand, march, and respond to orders in a ritual known as foot drill, which trains recruits to obey orders without hesitation or question. According to Finnish Army regulations,[citation needed] for example, the close-order drill:

  • Is essential for the esprit de corps and cohesion for battlefield conditions;
  • Gets the recruits used to instinctive obedience and following the orders;
  • Enables large units to be marched and moved in an orderly manner; and
  • Creates the basis for action in the battlefield.

In order to ensure that recruits will kill if ordered to do so, they are taught to objectify (dehumanize) their opponent as an ‘enemy target’ to ‘be engaged’, which will ‘fall when hit’. They are also taught the basic skills of their profession, such as military tactics, first aid, managing their affairs in the field, and the use of weaponry and other equipment. Training is designed to test and improve the physical fitness of recruits, although the heavy strain on the body also leads to a rate of injury.


Terms of service

Recruits enter a binding contract of service, which may differ according to rank, military branch, and whether the employment is full-time or part-time.


Minimum service period

Full-time military employment normally requires a minimum period of service of several years; between two and six years is typical of armed forces in Australia, the UK and the US, for example, depending on role, branch, and rank. The exception to this rule is a short discharge window, which opens after the first few weeks of training and closes a few months later, and allows recruits to leave the armed force as of right.


Part-time military employment, known as reserve service, allows a recruit to maintain a civilian job while training under military discipline for a minimum number of days per year in return for a financial bounty. Reserve recruits may be called out to deploy on operations to supplement the full-time personnel complement.


After leaving the armed forces, for a fixed period (between four and six years is normal in the UK and US, for example), former recruits may remain liable for compulsory return to full-time military employment in order to train or deploy on operations.


Military law

Military law introduces offenses not recognized by civilian courts, such as absence without leave (AWOL), desertion, political acts, malingering, behaving disrespectfully, and disobedience (see, for example, Offences against military law in the United Kingdom). Penalties range from a summary reprimand to imprisonment for several years following a court martial. Certain fundamental rights are also restricted or suspended, including the freedom of association (e.g. union organizing) and freedom of speech (speaking to the media). Military personnel in some countries have a right of conscientious objection if they believe an order is immoral or unlawful, or cannot in good conscience carry it out.


Posting and deployment

Personnel may be posted to bases in their home country or overseas, according to operational need, and may be deployed from those bases on exercises or operations anywhere in the world. The length of postings and deployments are regulated. In the UK, for example, a soldier is expected to be on deployment for no more than six months in every 30 months.These regulations may be waived at times of high operational tempo, however.


Perks

Perks of military service typically include adventurous training, subsidised accommodation, meals and travel, and a pension. Some armed forces also subsidise recruits' education before, during and/or after military service; examples are the St Jean military college in Canada, the Welbeck Defence Sixth Form College in the UK, and the GI Bill arrangements in the U.S. Conditions for participation normally apply, including a minimum period of formal military employment.


sources: wikipedia

AMX Leclerc Main Battle Tank




The Char Leclerc is a main battle tank (MBT) built by GIAT, now Nexter of France. It was named in honour of General Philippe Leclerc de Hauteclocque, who led the French element of the drive towards Paris while in command of the Free French 2nd Armoured Division (2e DB) in World War II.

The Leclerc is in service with the French Army and the army of the United Arab Emirates. In production since 1991, the Leclerc entered French service in 1992, replacing the AMX 30 as the country's main armoured platform. With production now complete, the French Army has 406 Leclerc and the United Arab Emirates Army has 388. The price in 2011 was €9.3 million, which made it the most expensive tank in history at the time. Following the devaluation of the Euro[clarification needed] its price fell dramatically, and in 2014 the K2 Black Panther surpassed the Leclerc's price record



Leclerc battle tank urban operations upgrade


In June 2006, Nexter unveiled the Leclerc optimised for urban operations. It is fitted with the AZUR kit, which consists of additional protection in the form of side skirts of composite material, bar armour on the rear of hull and turret to protect against rocket-propelled grenades (RPGs) and extra protection for the engine against petrol bombs.

A remotely controlled 7.62mm machine gun is also fitted in addition to the 120mm gun.

In early 2011, Nexter signed an agreement with the International Golden Group to supply Azur up-armour kits for the Leclerc MBTs of the UAE Armed Forces.
"The Leclerc was first operational with the French Army in 1992." 

FINDERS battle management system

The Leclerc is fitted with the FINDERS (fast information, navigation, decision and reporting system) battlefield management system, developed by Nexter Systems. FINDERS includes a colour map display which shows the positions of the host tank, allied and hostile forces and designated targets and can be used for route and mission planning.

The French Army has selected Nexter to equip its Leclerc main battle tanks with a terminal information system (TIS) called Icone (ergonomic communications and navigation interface). The initial phase of the contract covers the equipment of more than 100 Leclerc tanks.

The TIS has been developed together with EADS Defense Electronics Systems. It permits the exchange of digitised data including tactical situation and the graphic orders displayed on a background map, between the vehicle and higher level command. 

Leclerc main battle tank armament


The 120mm 52-calibre smoothbore gun is fitted with a thermal sleeve and muzzle reference system. Fumes are exhausted with a compressed air unit. The gun, which fires APFSD (armour-piercing fin-stabilised discarding sabot) and HEAT (high-explosive anti-tank) rounds, has a firing rate of 12 rounds a minute. The aiming system is entirely electrical for improved acceleration.

The tank has an automatic loading system, which allows cross-country fire-on-the-move against mobile targets. 22 rounds of ready-to-use ammunition are carried. The tank is also armed with a 12.7mm machine gun co-axial with the main gun and a roof-mounted 7.62mm anti-aircraft gun. 

The gunner's position, looking down from the turret roof.
Digital fire control and observation systems

The digital fire control system allows the gunner or commander to select six different targets to be engaged in just over 30 seconds. The system’s digital computer allows realtime treatment of data from the tank’s sensors and sights.

The commander has eight periscopes and an HL-70 stabilised panoramic sight from Safran (formerly SAGEM).
"In 2006, Giat unveiled the Leclerc optimised for urban operation."

HL-70 includes laser rangefinder, day channel, and second-generation image intensifier.

Recognition range is 4km and identification range is 2.5km. The commander has a display showing the gunner’s thermal sight. The gunner’s station is equipped with gunner’s main sight, three periscopes and a visual display unit. The gunner’s stabilised sight is SAVAN 20 from Safran, which contains a three-field-of-view thermal imager.

The driver’s station has three periscopes, of which the centre periscope is the OB-60 driver’s sight developed by Thales Optronique (formerly Thomson-CSF), which has day and night channels. 

Galix combat vehicle protection system


Leclerc is fitted with Galix combat vehicle protection system, developed by Nexter and Lacroix Tous Artifices. Nine launch tubes for the 80mm grenades are fitted on either side of the turret roof. The Galix system can launch smoke or anti-personnel grenades or infrared decoys.

Nexter has developed the KBCM defensive aids suite which can befitted to the Leclerc. KBCM includes laser warner, missile warner, infrared jammer and the Galix system and can be integrated with the FINDERS battle management system. The French Army has evaluated the system. 

SACM V8X-1500 Hyperbar diesel engine


The Leclerc is equipped with an SACM V8X-1500 Hyperbar diesel engine providing 1,500hp at 2,500rpm. An electronic engine management system is supplied by Safran. The SESM ESM 500 automatic transmission has a hydrostatic transmission unit and five forward and two reverse gears. The engine is fitted with a Suralmo-Hyperbar high pressure gas turbine. The engine provides a road speed over 70km/h and cross-country speed up to 50km/h.

The tank also has a Turbomeca TM-307B gas turbine auxiliary power unit. The hydropneumatic suspension system is from Societe d’Applications des Machines Motrices (SAMM). 

UAE tropicalised Leclerc main battle tank


The tropicalised Leclerc is optimised for tropical and desert conditions to meet the requirement of the UAE. A new powerpack and diesel auxiliary power unit has been installed and the hull is extended at the back to accommodate the powerpack and larger fuel tanks. The Euro Powerpack has the MTU 883 V-12 diesel engine providing 1,500hp, coupled with Renk HSWL295 TM automatic transmission. 

"Leclerc is fitted with Galix combat vehicle protection system."

For this and export versions of the tank, Nexter has developed the Leclerc Battle management equipment (LBME), a derivative of FINDERS. The HL-70 commander’s sight has been replaced by the HL-80, also from SFIM. 

Leclerc NGRV new-generation recovery vehicle


The Leclerc new-generation recovery vehicle (NGRV) has a longer hull with seven pairs of wheels.

A hydraulically operated blade at the front of the vehicle is used to clear a path through battlefield obstacles. The vehicle is equipped with an hydraulic crane rated to lift 30,000kg loads and a winch with 180m cable rated at 35,000kg. A secondary winch is rated at 1,500kg. The crane and winch systems are supplied by Rheinmetall Landsystemes GmbH.
 
Leclerc

Type Main battle tank
Place of origin France
Service history
In service 1993–present
Wars Yemeni Civil War (2015)
Production history
Designed 1983–1989
Manufacturer GIAT Industries (now Nexter)
Unit cost ₣rs104,304,000 in 1993, US$4+million in 2016 
Produced 1990–2008 (The last unit was produced in 2007 and the production line was closed, although Nexter retains the capability to build more if there is a need)
No. built ≈862
Specifications
Weight series 1: 54.5 tonnes
series 2: 56.3 tonnes
series XXI : 57.4 tonnes
Length 9.87 m (6.88 without gun )
Width 3.60 m
Height 2.53 m
Crew 3  (Commander, gunner, driver)

Armour modular composite armor
SXXI version include titanium, tungsten and semi-reactive layers.
Main
armament
GIAT CN120-26/52 120mm tank gun
40 rounds (1 round ready to fire in the chamber, 22 rounds inside the autoloader magazine with additional 18 rounds cylinder in the hull)
Secondary
armament
  • 12.7 mm coaxial M2HB machine gun (1,100 rounds)
  • 7.62 mm machine gun (3,000 rounds)
Engine 8-cylinder diesel SACM (Wärtsilä)
1,100 kW  (1,500 hp)
Power/weight 27.52 hp/tonne
Transmission Automatic SESM ESM 500
Suspension hydropneumatic
Fuel capacity 1300 liters (1700 ℓ with fuel drums)
Operational
range
550 km, 650 km (400 mi) with external fuel
Speed 72 km/h (45 mph)


T-80U Main Battle Tank



The T-80 is a third-generation main battle tank (MBT) designed and manufactured in the Soviet Union. When it entered service in 1976, it was the first MBT in the world to feature a powerful multifuel turbine engine as its main propulsion engine. The T-80U was last produced in a factory in Omsk, Russia, while the T-80UD and further-developed T-84 continue to be produced in Ukraine. The T-80 and its variants are in service in Belarus, Cyprus, Egypt, Kazakhstan, Pakistan, Russia, South Korea, and Ukraine. The chief designer of the T-80 was the Russian engineer Nikolay Popov.


T-80U main battle tank armament


The T-80U carries the 9M119 Refleks (Nato designation AT-11 Sniper) anti-tank guided missile system which is fired from the main gun. The range of the missile is 100m to 4,000m. The system is intended to engage tanks fitted with ERA (explosive reactive armour) as well as low-flying air targets such as helicopters, at a range of up to 5km. The missile system fires either the 9M119 or 9M119M missiles, which have semi-automatic laser beamriding guidance.

The tank is fitted with a 125mm 2A46M-1 automatic smoothbore gun with thermal sleeve, which can fire between 6 and 8 rounds/minute. Loading is hydro-mechanical with a 28 round carousel container. 45 rounds are carried. The gun fires separate loading projectiles which have semi-combustible cartridge case and sabot. Ammunition can be AP (armour piercing), APDS (armour piercing giscarding sabot), HEAT (high-explosive anti-tank) and HE-FRAG (high-explosive fragmentation).
"The T-80U carries the 9M119 Refleks (Nato designation AT-11 Sniper) anti-tank guided missile system."

Armament also includes a 7.62mm PKT coaxial machine gun and a 12.7mm Utes (NSVT-12.7) air defence machine gun. 


T-80U gunner position

Protection
The tank is protected by a combination of explosive reactive armour at the front and gill type armour panels elesewhere. Other countermeasures include quieter running, gas-turbine engine which exhausts smokeless gases, improved heat insulation of roof and hatches, ventilation of the engine-transmission system, cooling system, smoke-laying system and smoke discharging system.
Fire control and observation

The tank fire control system is the 1A42 which includes 1V517 ballistic computer, two-axis electrohydraulic weapon stabiliser, rangefinder sight stabilised in two axes as well as a GPK-59 hydro-semicompass azimuth indicator and an azimuth indicator for the turret rotation. This system permits firing on the move.

The gunner has the 1G46 day sight and also an infrared sight. 

Propulsion

The T-80U’s gas turbine engine is the GTD-1250 which produces 920kW (1,250hp). The GTD-1250 is a three shaft engine with two cascades of turbocompression. There is also an independent GTA-18 auxiliary power unit for use when the tank is stationary.

The tank has a planetary power transmission with hydraulic servo-system for increased mobility. The track and suspension system is fitted with RMSh track and rubber-tyred road wheels, torsion bar suspension with hydraulic telescopic double-acting shock absorbers. Maximum speed of the vehicle on road is 70km/h and across county is 48km/h. 

T-80U commander position


T-80UK command tank
The T-80UK tank provides command and control capability for field commanders and enable communications with superior command. It is similar to the T-80U but has a number of additional features. It is fitted with the Shtora-1 countermeasures suite also fitted on the T-90 tank. Shtora-1 is produced by Electronintorg of Russia. This system includes infrared jammer, laser warning system, grenade discharging system and a computerised control system. Operational range is 200m.
"The latest version of the T-80U being developed is the T-80UM2."

The tank has a combined symmetric dipole antenna for both UHF and HF communications. This increases range when the tank is stationary – up to 40km for the R-163-50U radio and 350 km for the R-163-50K radio. An AB-1-P28 1kW benzene generator is provided to power communications when the tank is stationary. T-80UK also has a more advanced fire control system, automatic loader for the gun, built-in turret ERA and TNA-4-3 navigational aid. 

T-80UM2

The latest version of the T-80U is the T-80UM2, also called Black Eagle or Chiorny Oriol, which is designed to engage targets while stationary or on the move. The demonstration of the prototype tank was held in Omsk in September 1997. The tank has a new all-welded cast steel turret with ERA on the hull front and turret, an automatic loading system and relocation of the ammunition to the turret bustle for improved survivability.

Other improvements include a computerised fire control system, thermal imaging sights for commander and gunner, and the Arena active countermeasures system. The T-80 UM2 is planned for exports.

 

T-80

Type Main battle tank
Place of origin Soviet Union
Service history
In service 1976–present
Used by See Operators
Wars First Chechen War, Second Chechen War, War in Donbass 
Production history
Designer Nikolay Popov, LKZ (T-80), KMDB (T-80UD)
Designed 1967–1975
Manufacturer LKZ and Omsk Transmash, Russia
Malyshev Factory, Ukraine
Unit cost USD $2.2 million T80U export, 1994.
Produced 1976–1992
No. built 5,404 (as of 2005)
Variants engineering & recovery, mobile bridge, mine-plough with KMT-6 plough-type system and KMT-7 roller-type system.
Specifications (T-80B / T-80U)
Weight 42.5 tonnes T-80B, 46 tonnes T-80U
Length 9.9 m (32 ft 6 in) T-80B, 9.654 m (31 ft 8.1 in) T-80U (gun forward)
7.4 m (24 ft 3 in) T-80B, 7 m (23 ft 0 in) T80U, (hull)
Width 3.4 m (11 ft 2 in) T-80B
3.603 m (11 ft 9.9 in) T-80U
Height 2.202 m (7 ft 2.7 in) T-80B, T-80U
Crew 3

Armour
  • T-80B : Hull 440-450 mm vs APFSDS 500-575 mm vs HEAT, Turret 500 mm vs APFSDS 650 mm vs HEAT
  • T-80U : Hull & Turret with Kontakt-5 780 mm vs APFSDS 1320 mm vs HEAT
Main
armament
125 mm 2A46-2 smoothbore gun,  36 rounds T-80B, 2A46M-1 with 45 rounds T-80U
9M112 Kobra ATGM, 4 missiles T-80B, 9M119 Refleks ATGM, 6 missiles T-80U
Secondary
armament
7.62 mm PKT coax MG, 12.7 mm NSVT or PKT antiaircraft MG
Engine SG-1000 gas turbine T-80B, GTD-1250 turbine T-80U, or one of 3 diesel T-80UD
1,000 hp T-80B, 1,250 hp T-80U
Power/weight 23.5 hp (17.6 kW) / tonne T-80B
27.2 hp (20.3 kW) / tonne T-80U
Transmission manual, 5 forward gears, 1 reverse T-80B, 4 forward, 1 reverse T-80U
Suspension torsion bar
Ground clearance 0.38 m (1.2 ft) T-80B, 0.446 m (1.46 ft) T-80U
Fuel capacity 1,100 litres (240 imp gal) (internal)
740 litres (160 imp gal) (external)
Operational
range
335 km (208 mi) (road, without external tanks)
415 km (258 mi) (road, with external tanks)
Speed 70 km/h (43 mph) (road)
48 km/h (30 mph) (cross country)


M1 Abrams Main Battle Tank




The M1 Abrams is an American third-generation main battle tank. It is named after General Creighton Abrams. Highly mobile, designed for modern armored ground warfare, the M1 is well armed and heavily armored. Notable features include the use of a powerful multifuel turbine engine, the adoption of sophisticated composite armor, and separate ammunition storage in a blow-out compartment for crew safety. Weighing nearly 68 short tons (almost 62 metric tons), it is one of the heaviest main battle tanks in service.

Three main versions of the M1 Abrams have been deployed, the M1, M1A1, and M1A2, incorporating improved armament, protection, and electronics. These improvements and other upgrades to in-service tanks have allowed this long-serving vehicle to remain in front-line service. In addition, development of the improved M1A3 version was first publicly disclosed in 2009. Extensive improvements have been implemeted to the latest M1A2SEPV3 version
Approved for production in 1990, the M1A2 represents the U.S. Army’s technological improvement of the basic M1A1 design and the most modern battle tank in the world. Outwardly similar in appearance to the M1A1, the most notable exterior changes on the M1A2 are the redesigned Commander's Weapon Station (CWS) and the addition of a Commander's Independent Thermal Viewer) on the left side of the turret forward of the loader's hatch. Internally, however, the M1A2 has been radically redesigned to take advantage of newer technology.


Most notable of these improvements is the addition of the Inter-Vehicle Information System (IVIS.) The IVIS system allows for the automatic and continual exchange of information between vehicles. By incorporating information provided by an on board Position/Navigation (POSNAV) system, unit commander's can track the location and progress of subordinate elements automatically, without tasking vehicle crews. In addition enemy positions can be identified, plotted and disseminated, while reports and artillery requests can be automatically formatted, transmitted, and processed. Lastly, map graphic control measures and operational orders can be rapidly distributed via the IVIS system.

To ensure information security, all IVIS data transmissions are routed through the M1A2's SINCGARS radio system. Improving on the "hunter-killer" tank commander-gunner target hand off method pioneered on the German Leopard II, the M1A2 takes this a step further by providing the Tank Commander with an independent thermal sight. This CITV sight allows the commander to independently scan for targets in all weather conditions and through battlefield obscurants. In addition to IVIS and the CITV, the M1A2 incorporates a number of additional electronic upgrades. Power distribution throughout the tank has been improved, relying on multiple bus paths so that in the event one conduit is damaged, power may still be delivered to a component via an alternate path. The driver's instrument display has been upgraded to a more detailed digital display and the Gunner's Primary Sight has been stabilized in two axes for increased accuracy.

Approved for implementation in 1995, the M1A2 SEP (System Enhancement Package) is a technology upgrade and standardization program, whereby the Army's fleet of M1s and M1A2s will all be brought to a common standard. Most notable among the modifications will be the introduction of a standard under armor auxiliary power unit and the addition a crew compartment air conditioning and cooling unit.

Other modifications within the vehicle will include upgrades to the IVIS system (color display, full size keyboard, digital mapping and graphics generation capability, and voice recognition capabilities), upgrades to the Gunner's Primary Sight assembly, and improvement in the tank's intercom and radio communications systems. Production of the M1A2 was halted after the initial run of 627 vehicles. As part of the fleet upgrade program, 547 of the Army's current inventory of M1s are being upgraded to M1A2 SEP standards, which will require the complete remanufacturing of the turret, while the current fleet of M1A2s will undergo a retrofit to bring them up to SEP standards.

 

M1 Abrams

Type Main battle tank
Place of origin United States
Service history
In service 1980–present
Used by See Operators below
Wars Persian Gulf War
War in Afghanistan
Iraq War
Iraqi Civil War
Saudi Arabian–led intervention in Yemen
Production history
Designer Chrysler Defense (now General Dynamics Land Systems)
Designed 1972–1979
Manufacturer Lima Army Tank Plant (since 1980)
Detroit Arsenal Tank Plant (1982–1996)
Unit cost US$6.21 million (M1A2 / FY99) Estimated in 2016 as US$8.92 million (with inflation adjustment)
Produced 1979–present
No. built approx. 10,000
Variants See variants
Specifications
Weight M1: 60 short tons (54 t)
M1A1: 63 short tons (57 t)
M1A2: 72 short tons (65 t)
Length Gun forward: 32.04 ft (9.77 m)
Hull length: 26.02 ft (7.93 m)
Width 12 ft (3.66 m)
Height 8 ft (2.44 m)
Crew 4 (commander/machine gunner, gunner, loader, driver)

Armor M1, M1A1: Burlington composite armor
M1A1HA, M1A2: depleted uranium mesh-reinforced composite armor
  • M1: Hull & turret –
    350 mm / 470 mm vs APFSDS,
    650 mm / 700 mm vs HEAT
  • M1A1: Hull & turret –
    600 mm vs APFSDS,
    700 mm vs HEAT
  • M1A1HA: Hull –
    600 mm vs APFSDS,
    700 mm vs HEAT,
    Turret –
    600 mm / 800 mm vs APFSDS,
    1,300  mm vs HEAT
Main
armament
M1: 105 mm L/52 M68 rifled gun (55 rounds)
M1A1: 120 mm L/44 M256A1 smoothbore gun (40 rounds)
M1A2: 120 mm L/44 M256A1 smoothbore gun (42 rounds)
Secondary
armament
1 × .50-caliber (12.7 mm) M2HB heavy machine gun with 900 rounds
2 × 7.62 mm (.308 in) M240 machine guns with 10,400 rounds (1 pintle-mounted, 1 coaxial)
Engine Honeywell AGT1500C multi-fuel turbine engine
1,500 shp (1,120 kW)
Power/weight From 26.9 hp/t (20.05 kW/t) to 23.8 hp/t (17.74 kW/t)
Transmission Allison DDA X-1100-3B
Suspension High-hardness-steel torsion bars with rotary shock absorbers
Ground clearance M1, M1A1: 0.48 m (1 ft 7 in)
M1A2: 0.43 m (1 ft 5 in)
Fuel capacity 500 US gallons (1,900 l; 420 imp gal)
Operational
range
M1A2: 426 km (265 mi)
Speed M1A1: Road 45 mph (72 km/h) (governed);
Off-road: 30 mph (48 km/h)
M1A2: Road 42 mph (67 km/h) (governed);
Off-road: 25 mph (40 km/h)


 sources: wikipedia, military