RQ-4 Global hawk

The Global Hawk UAV system comprises the RQ-4 air vehicle, which is outfitted with various equipment such as sensor packages and communication systems; and a ground element consisting of a Launch and Recovery Element (LRE), and a Mission Control Element (MCE) with ground communications equipment.[53] Each RQ-4 air vehicle 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 (910 kilograms). The fuselage comprises an aluminum, semi-monocoque construction with V-tail; the wings are made of composite materials.

There have been several iterations of the Global Hawk with different features and capabilities. The first version to be used operationally was the RQ-4A Block 10, which performed imagery intelligence (IMINT) with a 2,000 lb (910 kg) payload of a synthetic aperture radar (SAR) with electro-optical (EO) and infrared (IR) sensors; seven A-model Block 10s were delivered and all were retired by 2011. The RQ-4B Block 20 was the first of the B-model Global Hawks, which has a greater 3,000 lb (1,400 kg) payload and employs upgraded SAR and EO/IR sensors; four Block 20s were converted into communications relays with the Battlefield Airborne Communications Node (BACN) payload. The RQ-4B Block 30 is capable of multi-intelligence (multi-INT) collecting with SAR and EO/IR sensors along with the Airborne Signals Intelligence Payload (ASIP), a wide-spectrum signals intelligence (SIGINT) sensor. The RQ-4B Block 40 is equipped with the multi-platform radar technology insertion program (MP-RTIP) active electronically scanned array (AESA) radar, which provides SAR and moving target indication (MTI) data for wide-area surveillance of stationary and moving targets.

Since the RQ-4 is capable of conducting sorties lasting up to 30 hours long, scheduled maintenance has to be performed sooner than on other aircraft with less endurance. However, since it flies at higher altitudes than normal aircraft, it experiences less wear during flight

Corner shot

CornerShot is a weapon accessory invented by Lt. Col. Amos Golan of the Israeli Defense Forces in cooperation with American investors. It was designed in the early 2000s for SWAT teams and special forces in hostile situations usually involving terrorists and hostages. Its purpose is similar to that of the periscope rifle; it allows its operator to both see and attack an armed target, without exposing the operator to counterattack.

In the standard version a pistol is mounted in the front end of the weapon, which bends horizontally at a mid-gun sixty-degree hinge There is a digital camera and a flashlight attached to the barrel in the bayonet position. On the butt side of the hinge are the trigger, camera screen (which is on a horizontal hinge just like the mid-gun hinge but it is off of the left side of the gun), and controls for the camera and light.

Heckler & Koch MG5

The MG5 (formerly known as the HK121) is a general-purpose machine gun manufactured by Heckler & Koch. The weapon is intended as a replacement for the Rheinmetall MG3. The MG5 resembles the 5.56×45mm NATO Heckler & Koch MG4 light machine gun, which was adopted into German military service in 2005 The MG5 is gas-operated and chambered for the 7.62×51mm NATO round. 

The weapon's operation is almost similar to that of the MG4 light machine gun. The safety and three-position fire rate selector levers are ambidextrous, the butt stock can be folded depending on the variant, and numerous Picatinny rails allow installation of optical sights and other accessories. The quick-change barrel has a heat shield and a carrying/barrel exchange handle. A hot barrel can be replaced without protective gloves. The iron sights consist of a collapsible front sight and a height and windage adjustable rear diopter sight.

 The charging handle is on the right side of the weapon. For feeding, 50-round belted ammunition pouches or 120-round belted ammunition boxes can be mounted on the left side. The MG5 can be installed on all mounts and tripods originally developed for MG3 machine guns, using additional adapters
compiled by XENOCIDE

Puma (IFV)

The Puma is a German infantry fighting vehicle (Schützenpanzer or short SPz) designed to replace the aging Marder IFVs. The company responsible for the project is PSM Projekt System Management, a joint venture of Krauss-Maffei Wegmann and Rheinmetall Landsysteme. The Puma is one of the best-protected IFVs, while still having a high power-to-weight ratio. The Puma, while externally not very different from existing IFVs, incorporates a number of advances and state-of-the-art technologies.

The most obvious of these is the incorporated ability to flexibly mount different armour . Another feature is the compact, one-piece crew cabin that enables direct crew interaction ("face-to-face"; like replacing the driver or gunner in case of a medical emergency) and minimizes the protected volume. The cabin is air conditioned, NBC-proof with internal nuclear and chemical sensors and has a fire suppressing system using non-toxic agents. The engine compartment has its own fire extinguishing system. The only compromise of the otherwise nearly cuboid cabin is the driver station, located in a protrusion in front of the gunner, in front of the turret.

 One measure to achieve the one-piece cabin is the use of an unmanned, double-asymmetrical turret : while slightly off-center turrets are common in IFVs, the Puma's turret is on the left-hand side of the vehicle, while the main cannon is mounted on the right side of the turret and thus on the middle axis of the hull when the turret is in the forward position. The outer hull (minus the turret) is very smooth and low to minimize bullet traps and the general visual signature.

 The whole combat-ready vehicle in its base configuration will be air transportable in the Airbus A400M tactical airlifter. Its 3+6 persons crew capability is comparable to other vehicles of comparable weight, like the US American M2 Bradley IFV, the same as in the Marder, but smaller than the 3+8 of the CV9030 and CV9035.compiled by XENOCIDE

Sukhoi Su-25

The All versions of the Su-25 have a metal cantilever wing, of moderate sweep, high aspect ratio and is equipped with high-lift devices. The wing consists of two cantilever sections attached to a central torsion box, forming a single unit with the fuselage. The air brakes are housed in fairings at the tip of each wing. Each wing has five hardpoints for weapons carriage, with the attachment points mounted onload-bearing ribs and spars. Each wing also features a five-section leading edge slat, a two-section flap and an aileron.
The flaps are mounted by steel sliders and rollers, attached to brackets on the rear spar. The trapezoidal ailerons are near the wingtips.The fuselage of the Su-25 has an ellipsoidal section and is of semi-monocoque, stressed-skin construction, arranged as a longitudinal load-bearing framework of longerons, beams and stringers, with a transverse load-bearing assembly of frames. The one-piece horizontal tailplane is attached to the load-bearing frame at two mounting points has a conventional aerodynamic layout with a shoulder-mounted trapezoidal wing and a traditional tailplane and rudder. Several metals are used in the construction of the airframe: 60% aluminium, 19% steel, 13.5% titanium, 2% magnesium alloy and 5.5% other materials. All versions of the Su-25 have a metal cantilever wing, of moderate sweep, high aspect ratio and is equipped with high-lift devices. 

The wing consists of two cantilever sections attached to a central torsion box, forming a single unit with the fuselage. The air brakes are housed in fairings at the tip of each wing. Each wing has five hardpoints for weapons carriage, with the attachment points mounted on load-bearing ribs and spars. Each wing also features a five-section leading edge slat, a two-section flap and an aileron. The flaps are mounted by steel sliders and rollers, attached to brackets on the rear spar. The trapezoidal ailerons are near the wingtips.

 The fuselage of the Su-25 has an ellipsoidal section and is of semi-monocoque, stressed-skin construction, arranged as a longitudinal load-bearing framework of longerons, beams and stringers, with a transverse load-bearing assembly of frames. The one-piece horizontal tailplane is attached to the load-bearing frame at two mounting points
compiled by XENOCIDE

Sikorsky CH-53E Super Stallion

The Sikorsky CH-53E Super Stallion is the largest and heaviest helicopter in the United States military. As the Sikorsky S-80 it was developed from the CH-53 Sea Stallion, mainly by adding a third engine, adding a seventh blade to the main rotor and canting the tail rotor 20 degrees. It was built by Sikorsky Aircraft for the United States Marine Corps.

 Although dimensionally similar, the three engine CH-53E Super Stallion or Sikorsky S-80 is a much more powerful aircraft than the original Sikorsky S-65 twin engined CH-53A Sea Stallion. The CH-53E also added a larger main rotor system with a seventh blade.

 The CH-53E can transport up to 55 troops or 30,000 lb (13,610 kg) of cargo and can carry external slung loads up to 36,000 lb (16,330 kg). 

The Super Stallion has a cruise speed of 173 mph (278 km/h) and a range of 621 miles (1,000 km).The helicopter is fitted with a forward extendable in-flight refueling probe and it can also hoist hose refuel from a surface ship while in hover mode. 

It can carry three machine guns: one at the starboard side crew door; one at the port window, just behind the copilot; and one at the tail ramp.The CH-53E also has chaff-flare dispensers 

                                                          compiled by XENOCIDE

Ilyushin Il-76

The Ilyushin Il-76 (NATO reporting name: Candid) is a multi-purpose four-engine turbofan strategic airlifter designed by the Ilyushin design bureau. It was first planned as a commercial freighter in 1967, as a replacement for the Antonov An-12. It was designed to deliver heavy machinery to remote, poorly served areas of the USSR.

 Military versions of the Il-76 have been widely used in Europe, Asia and Africa, including use as an aerial refueling tanker or command center. The Il-76 has seen extensive service as a commercial freighter for ramp-delivered cargo, especially for outsized or heavy items unable to be otherwise carried. It has also been used as an emergency response transport for civilian evacuations as well as for humanitarian aid and disaster relief around the world. 

Because of its ability to operate from unpaved runways, it has been useful in undeveloped areas. Specialized models have also been produced for aerial fire-fighting and zero-G training. The aircraft was first conceived by Ilyushin in 1967 to meet a requirement for a freighter able to carry a payload of 40 tons (88,000 lb) over a range of 5,000 km (2,700 nmi; 3,100 mi) in less than six hours, able to operate from short and unprepared airstrips, and capable of coping with the worst weather conditions likely to be experienced in Siberia and the Soviet Union's Arctic regions. compiled by XENOCIDE

Antonov AN 32

The An-32 is basically a re-engined An-26. The launch customer was the Indian Air Force, which ordered the aircraft partly due to good relations between then USSR leader Leonid Brezhnev and then India leader Indira Gandhi. The An-32 is designed to withstand adverse weather conditions better than the standard An-26. The high placement of the engine nacelles above the wing allowed for larger diameter propellers, which are driven by 5,100 hp rated AI-20 turboprop engines, providing almost twice the power of the An-26's AI-24 powerplants. Estimated price for a modernised An-32 version is 15 million dollars

The AN-32 light military transport multi-purpose aircraft can be operated in various climate conditions, including hot climate (up to + 50°C) and from the mountain airfields (up to 4500 m elevation). The main aircraft purpose is to transport cargoes over short and medium range air routes.

It can be used for carrying military personnel, aerial delivery of paratroopers and palletized and non-palletized cargoes.
compiled by XENOCIDE

Magpul FMG-9

The Magpul FMG-9 is a prototype for a generation of folding submachine guns having cartrigde of 9x19 parabellum, designed by Magpul Industries in 2008. 

Like other folding machine guns, it would be used for concealed carry and can be disguised as anything from a small package to an extra laptop battery. It is made out of a light-weight polymer material rather than metal, making it very light and easy to carry. It is also small enough even to fit in the back pocket of most everyday pants. 

It was developed for potential use by personal protection details such as the United States Secret Service.
compiled by XENOCIDE

Merkava mkIV

The Mark IV is the most recent variant of the Merkava tank that has been in development since 1999 and production since 2004. The upgrade's development was announced in an October 1999 edition of the Bamachaneh ("At the Camp") military publication. However, the Merkava Mark III remained in production until 2003. The first Merkava IVs were in production in limited numbers by the end of 2004. The model has a new fire-control system, the El-Op Knight Mark 4. Removable modular armor, from the Merkava Mark IIID, is used on all sides, including the top and a V-shaped belly armor pack for the underside.

This modular system is designed to allow for damaged tanks to be rapidly repaired and returned to the field. Tank rounds are stored in individual fire-proof canisters, which reduce the chance of cookoffs in a fire inside the tank. The turret is "dry": no active rounds are stored in it. Some features, such as hull shaping, exterior non-reflective paints, and shielding for engine heat plumes mixing with air particles to confuse enemy thermal imagers, were carried over from the IAI Lavi program of the Israeli Air Force to make the tank harder to spot by heat sensors and radar. The Mark IV includes the larger 120 mm main gun of the previous versions, but can fire a wider variety of ammunition, including HEAT and sabot rounds like the APFSDS kinetic energy penetrator, using an electrical semi-automatic revolving magazine for 10 rounds.

It also includes a much larger 12.7 mm machine gun for anti-vehicle operations (most commonly used against technicals). The Mark IV has the Israeli-designed "TSAWS (Tracks, Springs, and Wheels System)" caterpillar track system, called "Mazkom" by troops. This system is designed to reduce track-shedding under the harsh basalt rock conditions of Lebanon and the Golan Heights. The tank carries the Israeli Elbit Systems BMS (Battle Management System), a centralised system that takes data from tracked units and UAVs in theater, displays it on color screens, and distributes it in encrypted form to all other units equipped with BMS in a given theater.

 The Merkava IV has been designed for rapid repair and fast replacement of damaged armour, with modular armour that can be easily removed and replaced. It is also designed to be cost-effective in production and maintenance; its cost is lower than that of a number of other tanks used by Western armies.
compiled by XENOCIDE

Mikoyan Gurevich MiG 25 foxbat interceptor

The Mikoyan-Gurevich MiG-25 is a supersonic interceptor and reconnaissance aircraft that was among the fastest military aircraft to enter service. It was designed by the Soviet Union's Mikoyan-Gurevich bureau. The first prototype flew in 1964, and the aircraft entered service in 1970. It has an operational top speed of Mach 2.83 (Mach 3.2 is possible but at risk of significant damage to the engines), and features a powerful radar and four air-to-air missiles. Because of the thermal stresses incurred in flight above Mach 2, the Mikoyan-Gurevich OKB had difficulties choosing what materials to use for the aircraft.

They had to use E-2 heat-resistant Plexiglas for the canopy, and high-strength stainless steel for the wings and fuselage. Using titanium rather than steel would have been ideal, but it was expensive and difficult to work with.

The problem of cracks in welded titanium structures with thin walls could not be solved, so the heavier nickel steel was used instead. It cost far less than titanium and allowed for welding, along with heat resistant seals. The MiG-25 was constructed from 80% nickel steel alloy, 11% aluminium, and 9% titanium.The steel components were formed by a combination of spot welding, automatic machine welding and hand arc welding methods

MiG-27

The Mikoyan MiG-27 is a variable-geometry ground-attack aircraft, originally built by the Mikoyan design bureau in the Soviet Union and later license-produced in India by Hindustan Aeronautics as the Bahadur ("Valiant"). It is based on the Mikoyan-Gurevich MiG-23 fighter aircraft, but optimized for air-to-ground attack. Unlike the MiG-23, the MiG-27 did not see widespread use outside Russia, as most countries opted for the MiG-23BN and Sukhoi Su-22 instead. It currently only remains in service with the Indian, Kazakh and Sri Lankan Air Forces in the ground attack role

The MiG-27 shares the basic airframe of the MiG-23, but with a revised nose – nicknamed "Utkonos" ("Platypus") in Russian service, first introduced on the MiG-23B. Dissatisfaction with the MiG-23BN led to the further development of the basic airframe to accommodate a stronger undercarriage, simpler intakes and a shorter exhaust nozzle, without radar in favor of a downward-sloping profile for improved pilot visibility, a laser rangefinder and marked-target seeker. Among its test pilots, it was also called "Balkon" ("Balcony") because of the increased frontal view from the cockpit. Additional cockpit armor was installed, along with a totally new nav/attack system. Since the MiG-27 was intended to fly most of its missions at low altitude, the MiG-23's variable intake ramps and exhaust nozzles were discarded in favor of a simpler fixed configuration, reducing weight and maintenance requirements.

The aircraft also has larger, heavy-duty landing gear to facilitate operation from poorer-quality airfields. In accordance with the MiG-27s strike and low-level attack requirements, provisions were made to mount missiles and precision-guided munitions, as well as retaining a nuclear capability in line with other Soviet combat aircraft by introducing specialized navigation system
compiled by XENOCIDE