The Polish army has showed the interest of a new fire support vehicle based on the Rosomak 8×8 armoured vehicle which is the standard wheeled armoured vehicle uses by the Polish Armed Forces. With this type of vehicle, the Polish army will have an high mobility vehicle with fire power of a main battle tank.
The Cockerill 120mm high pressure gun provides a strengthened anti-armour capability. This weapon fires all NATO-standard 120mm smoothbore ammunition and the Falarick 120 GLATGM, which permits the effective engagement and penetration of heavy armour to beyond 5km range.
120mm Compact L44 by RUAG
Both guns are employed using a common high performance, digital, fully-stabilised, day/night weapon control system. Turret weight is kept low through the use of a bustle-mounted autoloader, which permits a two-person crew. The Cockerill XC-8 concept-turret draws on the proven modular technology of the Cockerill CT-CV 105HP turret and may be realised at low risk.
The Cockerill XC-8 concept-turret promises a significant advance in terms of medium-weight direct-fire capability. The combination of highly effective and flexible lethality options with outstanding strategic and tactical mobility, opens up a new range of operational possibilities
Material source: Pakistan Defence
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Note: There is not much info as it is a concept
The 120mm seems to be the same used on the CV90 120-T a Compact L44 by RUAG
The Beriev Be-200 is a multipurpose amphibious aircraft manufactured by Russia-based Irkut. The aircraft was developed under Irkut’s first full-scale civil programme. The Be-200 cooperation programme includes key aviation industry companies such as Beriev Aircraft, Airbus, EADS-Irkut Seaplane (EISP) and EADS.
Beriev rolls out first serial-produced Be-200Chs amphibious multirole aircraft:Here
Beriev rolled out the first upgraded Be-200Chs amphibious aircraft (Credit: UAC)
The Be-200 can be configured for fire fighting, search and rescue, maritime patrol and environmental monitoring, cargo and passenger transportation operations. It can take off and land on unprepared airstrips and water.
Alexxx Malev
The first Be-200 test aircraft completed its maiden flight in September 1998. Be-200ES, the first production aircraft, touched the skies in June 2003. The Russian Ministry of Emergency Situations (Emercom) was the first customer to receive an aircraft in July 2003 under seven Be-200 fire-fighting and rescue aircraft order. The Ministry of Emergencies, Azerbaijan, took the delivery of one Be-200ES aircraft in 2008.
Alexey Kachaev
The Russian Navy plans to procure four Be-200 aircraft for reconnaissance and search and rescue duties, with deliveries scheduled between 2010 and 2013. The People’s Liberation Army Navy (PLAN) of China is also in discussions with Russia to buy the maritime search and rescue variant.
Beriev Be-200 amphibious aircraft design
Alexander Shatsky – AviMedia
The aircraft was designed by Beriev Aircraft and is assembled at the Irkutsk Aviation Plant of Irkut.
Designed as a multirole amphibious platform, the Be-200 can be configured for a range of missions. The aircraft is a high-wing T-tail monoplane with a single-step design hull. The design provides stability in water.
Valentin Lozovik – AviMedia
The airframe is made of aluminium alloys and coated with corrosion-protection materials. The Be-200 features significant maritime characteristics to perform littoral and blue water operations. The aircraft delivers flight characteristics similar to conventional aircraft.
Be-200 mission variants
Arina Shamova
The baseline design of Be-200 amphibious aircraft is intended for aerial wildfire-fighting using water or fire-extinguishing liquids. This includes the following objectives:
Stopping the spread, and containment, of moderate and large forest fires by creating a barrier with multiple drops of an extinguishing fluid at the edge of the fire;
The elimination of small and newly-started forest fires; the delivery of firefighting teams and equipment to disaster areas with landing on a preselected water surface or airfield, and subsequent extraction.
Maiya Sokolova – AviaPressPhoto
Additionally, the airplane can perform:
passenger transportation;
search-and-rescue work;
environmental monitoring;
patrolling of exclusive economic zones and sea boundaries.
The Be-200 can be reequipped into the following versions quickly and with minimum cost:
transport airplane;
passenger airplane (Be-210);
search-and-rescue airplane;
medical evacuation airplane.
Source uacrussia.ru
Firefighting version
Aleksander Markin. Александр Маркин
redstar.gr
Lera Kiame
Passenger
Igor Kolokolov
Search-and-rescue version
The Be-200 mission variants include fire-fighting, search and rescue, freighter, passenger aircraft and ambulance. The fire-fighting variant has a crew of two members, and is fitted with fire extinguishing fluid and water tanks. The aircraft can drop 270t of water on the fire area without refuelling.
Anatoly Sergunin – AviaPressPhoto
The search and rescue (SAR) variant can perform operations within an area of 200 miles for 6.5 hours. The aircraft is equipped with an inflatable rubber dinghy, thermal-imaging and optical search aids and first-aid kit. The SAR variant can be configured to carry 45 passengers.
Aleksander Markin. Александр Маркин
Aleksander Markin. Александр Маркин
The transport variant is fitted with floor-mounted cargo-handling equipment to transport loose cargoes, as well as cargoes loaded in standard containers and pallets. The aircraft has the capacity to carry 6.5t payload.
Aleksander Markin. Александр Маркин
The passenger variant, designated as Be-210, can carry 72 passengers. It has the maximum range of 1,850km.
The BE-200 ambulance version can accommodate ten medical staff as well as 30 injured persons on stretchers. The aircraft feature emergency diagnostics and intensive care facilities.
Be-200 cockpit
Sergey Popkov
The Be-200 is equipped with a partial glass cockpit. The cockpit features a digital flight control (fly-by-wire) system and modern navigation systems, including satellite navigation (GPS), flight management system (FMS), autopilot and weather radar.
The flight control system, integrated with an aerodynamic design, provides high maneuverability at low speeds as well as better handling capabilities and safety, and reduces the pilot’s workload.
Be-200 avionics suite
Andrey Bagirov
The Be-200 integrates a full suite of avionics for all weather requirements. The ARIA 200-M all-weather integrated avionics system features six large LCDs. The system is developed by Honeywell along with the Moscow Research Institute of Aircraft Equipment.
ARIA 200-M all-weather integrated avionics system
kret.com
The high level of technological innovation and the world-class parameters of the new development led to the ARIA-200 system being included in Russia’s newest amphibious aircraft, the Be-200ChS, and its certification both in Russia (IAC AR) and Europe (EASA). It thus met both current and future requirements for international air navigation.
Since 2001, the system has been successfully used by Be-200ChS aircraft, and its modifications and related systems have been installed on Il-114-100, Il-96-300/400, Tu-204-100/300, and Tu-214 aircraft. During this period, the system was continually improved to include other functional tasks and ensure compliance with newly introduced international standards. In 2015, experts from the institute completed work on a significant modernization of the avionics installed on the Be-200ChS.Source kret.com
Be-200 Head-Up Display System
beriev.com
Yet another line in the upgrading of the airborne equipment of Be-200 aircraft is the installation in Be-200 cockpit of the Head-Up Display System of SAAB development. Apart from this, the aircraft will be equipped with a visual-range monitoring video camera and with an IR-camera to be mounted over the windshield, the data from which will be displayed on the head-up display.
A similar system has already been tested on the prototype Be-200 amphibious aircraft, and may, upon the customer’s request, be installed on the aircraft being manufactured as well as on serial amphibious aircraft already in operation.Source beriev.com
High-bypass ratio engines
Laith Jobran @flickr
The aircraft is powered by two D-346TP high-bypass ratio engines, a TA 12-60 auxiliary power unit, an engine control system and engine vibration monitoring system. The D436TP turbofan engines deliver a higher performance at hot-and-high conditions compared with turboprop engines installed on similar types of fire-fighting aircraft. The engines have been developed with advanced materials and innovative solutions.
2 x D-346TP high-bypass ratio engines
Low SFC and low weight-to-thrust ratio;
High reliability due to long experience in operating the D-36 engine of similar class;
Low noise and emissions;
Easy maintenance, high efficiency of the monitoring and diagnostics system;
Steady operation in event of sudden airflow temperature inversions at engine inlet when fighting forest fires;
Availability of multi-purpose engine mounts allowing for installation in various aircraft on underwing or overwing pylons, in fuselage or on either side of the fuselage without any changes in the engine design;
Operability in maritime conditions;
Low operating costs and long service life.
Alexandr Meshkov
TA-12A APU
TA12-60 is a single-shaft auxiliary gas-turbine engine with the equivalent power of 360 kWt. This engine is designed for aircraft and helicopter APUs. It is used for air turbine start of the helicopter and aircraft mid-flight engines, AC electric power of 115/200 V, power up to 60 kWA and providing air conditioning for cockpit and cabins.
High overall efficiency of the engine is based on the use of a 4-stage axial compressor. An annular reverse-flow combustion chamber of evaporative type provides 0,99 burning and low content of hydrocarbons in the exhaust gases. The engine contains a 3-stage axial turbine. Driving units, including alternator, are installed on the engine’s gearbox.
seawings.co.uk
The noise level of the TA12-60 engine, when installed on the craft, does not exceed 90 dB.
The engine complies with the Norms of Aircraft Airworthiness (NLGS-3); this is confirmed by a type certificate No 101-VD issued by the Aviation Register of the IAC.
Since 2005 the TA 12-60 APU has been operated under the second strategy. The TA 12-60 APU is operated subject to the technical condition till the specified life time of the principle components is terminated (4,000 hr/starts).
The TA12-60 engine has been in serial production since 1996.
Development: PowerJet – joint venture between NPO Saturn and Snecma (SAFRAN Group, France)
Production: NPO Saturn and Snecma in accordance with the agreed work sharing*
SaM146 – integrated power plant (comprising turbofan engine, nacelle with thrust reverser, equipment) for new generation regional-mainline aircraft. * The work sharing: • Snecma: core, accessory drive, control system, power plant integration, flight tests • NPO Saturn: fan, low pressure module, final engine assembly, ground tests
Design features
• fan with wide chord blades • 3-stage low pressure compressor • 6-stage high pressure compressor • annular combustor • 1-stage high pressure turbine • 3-stage low pressure turbine
Application
The first application of SaM146 is the Sukhoi Superjet 100 aircraft family, created by Sukhoi Civil Aircraft Company (UAC, Russia) in cooperation with Alenia Aermacchi (Finmeccanica, Italy): • SaM146-1S17 for SSJ100-95B regional jet • SaM146-1S18 for SSJ100-95LR regional jet and SBJ business jet
Advantages
Compact, reliable, efficient and eco-friendly engine, based on combination of advanced and proven technologies, Western and Russian engine-building expertise: • certified in accordance with EASA and IAC AR standards • wide range of thrust • high reliability (on a par with CFM56 standard) • meets the ICAO ecological standards • full commonality within aircraft family • low cost of ownership
SaM146 power plant and all after-sale services are delivered by PowerJet SA.
The aircraft is equipped with hydraulically operated rearward retractable landing gear units. Each unit has two wheels in addition to a water rudder, which provides steering in the water. The underwing stabiliser floats fitted on wings provide stability in water.
seawings.co.uk
Be-200 aircraft performance
llya Solovey
The Be-200 can fly at a maximum speed of 680km/h. It has a range of 3,300km and service ceiling of 8,000m. The aircraft can climb at a rate of 3,350ft per minute. The Be-200’s maximum take-off weight on the runway and water is 41t and 37.9t respectively.
UAC Russia
Specification
Be-200
Be-200ChS
Dimensions
Wing span (m)
32,78
Aircraft lenght (m)
32,05
Aircraft height (m)
8,9
Wing area (m2)
117,44
Wing sweep angle at 1/4 chord line (degrees)
23`
Fuselage diameter (m)
2,86
Wheel track (m)
4,3
Engine’s main performance data
Engine type and model
D436-TP
Number of engines
2
Maximum takeoff thrust (ISA, H=0) (kgf)
2х7500
Maximum unboosted thrust (ISA, H=0) (kgf)
2х1500
Fuel consumption (kg/kgf·h (kg/N·h))
0,608 (0,062)
Weight characteristics
Maximum take-off weight (kg)
runway – 37900
runway – 42000
water – 37200
water – 40000
Max payload (weight of water loaded to tanks) (kg)
12000
Empty weight(kg)
25340
28000
Total capacity of fuselage fuel tanks (l)
12500
Performance data
Flight speed (km/h)
710
700
Maximum flight range (km)
3600
3100
Maximum range with maximum payload (km)
1400
1800
Take-off distance (land/water) (m)
700/1000
1350/1000
Landing distance (land/water) (m)
950/1300
1020/1300
flight altitude (m)
8000
Seaworthiness
Seaworthiness, sea state
3
Wave height (m)
up to 1,2
Min depth required for operation (m)
2,6
Cargo cabin dimensions
Length (m)
18,7
Height (m)
1,9
Maximum width (m)
2,5
Floor area (m2)
41
Volume (m3)
80,8
Service life
Calendar
30
Fire suppression
Maximum capacity of water tanks (m3)
12
Maximum capacity of chemical fluid (m3)
1,2
Rate of climb after water scooping by skimming (43 t, sea level) (m/s)
This fixed-wing aircraft, a modified version of the Tupolev Tu-214 airliner, has been developed especially for the Presidential Executive Office.
Tupolev Tu-214SR, a modified version of the Tu-214, is the Russian so called ‘Doomsday Plane.’ Outfitted with a state-of-the-art multi-intelligence payload, it was designed to provide the Russian leadership with a mobile command and control center in case of a major cataclysm or a global war. Source sputniknews.com
While significantly less is known about capabilities of the 214SR than the E-4B , we do know that it carries an MRC-411 multi-intelligence payload, which includes electronic intelligence (ELINT) sensors, side-looking Synthetic Aperture Radar (to spot incoming air threats from long range), and a variety of Signals Intelligence (SIGINT) and Communications Intelligence (COMINT) equipment. Four onboard generators provide ample amperage while a set of external fuel tanks allow the plane to remain aloft for trips up to 10,000 km.
Image: From the netImage: From the net
The two such 214SRs entered service in 2008 with the Presidential Special Applications Squad and are operated by a crew of four. However, the plane was only declassified last year when it made its public debut at the Moscow Air Show. Since then, it’s been spotted in the skies above both the Sochi Olympics, and more recently—and ominously—in Crimea. Source gizmodo.com
Tu-214 SR was especially developed for use by the President of the Russian Federation as commanding airborne center.
The first flight took place in 2008 and is a modified Tu-214.
Externally Tu-214 SRdiffers from its aerodynamic cover on the top of the fuselage. It can accommodate up to 62 persons and has extended electric power resources since 4 generators were added on it.
The crew is now 4 persons (instead of 2) and its range was increased from 7,000 to 10,000 km due to use of external fuel tanks.
It’s first flight of Tu-214 SR (RA-64515) was performed in April 27, 2008, while the second prototype with serial number RA-64516 first flew in December 10, 2008. Both were delivered on June 1, 2009 and were incorporated in the Presidential Special Applications Squad.
The new Tu-214 SR replaced the aged Il-18, which had stayed in service for over 40 years.
The Boeing (McDonnell Douglas) (formerly Hughes) AH-64A Apache is the Army’s primary attack helicopter. It is a quick-reacting, airborne weapon system that can fight close and deep to destroy, disrupt, or delay enemy forces. The Apache is designed to fight and survive during the day, night, and in adverse weather throughout the world.
The principal mission of the Apache is the destruction of high-value targets with the HELLFIRE missile. It is also capable of employing a 30MM M230 chain gun and Hydra 70 (2.75 inch) rockets that are lethal against a wide variety of targets. The Apache has a full range of aircraft survivability equipment and has the ability to withstand hits from rounds up to 23MM in critical areas.
The AH-64 Apache is a twin-engine, four bladed, multi-mission attack helicopter designed as a highly stable aerial weapons-delivery platform. It is designed to fight and survive during the day, night, and in adverse weather throughout the world. With a tandem-seated crew consisting of the pilot, located in the rear cockpit position and the co-pilot gunner (CPG), located in the front position, the Apache is self-deployable, highly survivable and delivers a lethal array of battlefield armaments. The Apache features a Target Acquisition Designation Sight (TADS) and a Pilot Night Vision Sensor (PNVS) which enables the crew to navigate and conduct precision attacks in day, night and adverse weather conditions.
PilotWSO
An on-board video recorder has the capability of recording up to 72 minutes of either the pilot or CPG selected video. It is an invaluable tool for damage assessment and reconnaissance. The Apache’s navigation equipment consists of a doppler navigation system, and most aircraft are equipped with a GPS receiver.
The U.S. Army is developing a Version 6 update of the Boeing AH-64E Apache that by 2018 will enhance its fire-control radar, expand its ability to communicate with unmanned aircraft and soldiers on the ground, and increase onboard processing speeds. The work was underway as the service sought approval for its first multi-year procurement of the fearsome attack helicopter.
The “heavily software dependent” Version 6 capabilities will be implemented on the latest-model Apache by April 2018 at a cost of $298.5 million, according to a “Justification and Approval” document signed in April 2015 by Heidi Shyu, the Army’s senior procurement executive.
AUSA 2016: US Army to complete AH-64E Version 6 and MUM-TX operational testing this year:Here
Excerpt:
Meanwhile, the Version 6 improvements for the AH-64E are expected to include a new maritime targeting mode, as well as aided target detection/classification; multimode laser image blending; a radar frequency interferometer (RFI); passive ranging/range extension; fire-control radar enhancements; Longbow integrated maintenance support system ground analysis software improvement; an interactive electronic technical manual upgrade; and Soldier Radio Waveform (SRW) embedded diagnostics. The upgrades are designed to be retrofittable onto the aircraft at the unit location.
The Apache has state of the art optics that provide the capability to select from three different target acquisition sensors. These sensors are:
– Day TV. Views images during day and low light levels, black and white.
– TADS FLIR. Views thermal images, real world and magnified, during day, night and adverse weather.
– DVO. Views real world, full color, and magnified images during daylight and dusk conditions.
Prominent in this picture, on the nose of the aircraft, is the day TV system, thermal imaging sight and direct view optics. All of these aid the pilot and co-pilot in acquiring and engaging multiple targets simultaneously in different environments. Photo by Peter Davies Crown Copyright
Image @media.defenceindustrydaily.com
Arrowhead® Modernized TADS/PNVS Receiver for the Apache
Identify targets and deliver high quality images, right into a pilot’s helmet display. In real time. In any condition.
This mission-critical receiver integrates within the Modernized Target Acquisition Designation Sight (M-TADS) as well as the Modernized Pilot Night Vision Sensor (M-PNVS), to help ensure safe flight in the most blinding conditions. With real-time high quality images, pilots can avoid difficult-to-detect obstacles, like wires, during low-altitude flights. Even in complete darkness.
With enhanced reliability and streamlined field maintenance, operation and support costs have also been lowered by as much as 60 percent. Source drs.com
AUSA 2016: US Army awards Lockheed Martin USD49 million for Apache sensor upgrade work:Here
Excerpt
The US Army has awarded Lockheed Martin a USD49.3 million contract to upgrade the Modernized Target Acquisition Designation Sight/Pilot Night Vision Sensor (M-TADS/PNVS) on the Boeing AH-64E Apache helicopter, the company announced on 3 October.
Lockheed Martin is responsible for producing 42 Modernized Day Sensor Assembly (M-DSA) upgrade kits and spares as part of Lot 1 production under the deal. M-DSA provides the ability to more rapidly identify targets and co-ordinate with troops on the ground. Its modular design also reduces operation and support costs, according to Lockheed Martin.
Lockheed Martin receives a $337 million contract to supply new M-TADS/PNVS for Apache attack helicopters:Here
Excerpt
The AH-64E Apache helicopter is slated to receive new eyes as Lockheed Martin receives a $337 million contract to supply multiple countries with the latest in target acquisition.
The Modernized Target Acquisition Designation Sight/Pilot Night Vision Sensor or M-TADS/PNVS system has been ordered by the United States, United Kingdom and the Kingdom of Saudi Arabia, the company announced on Monday..
M-DSA
The Modernized Day Sensor Assembly (M-DSA) is currently in production and modernizes the M-TADS/PNVS system. It brings color to the Apache cockpit.
High Reliability Turret
The High Reliability Turret will replace the legacy TADS turret assembly as the structure that interfaces with the Apache aircraft and houses the M-TADS/PNVS sensors. It also houses the motors that drive the azimuth and elevation movement of the sensors. High Reliability Turret provides reliability and maintainability improvements, resulting in operation and support cost savings of more than $695 million over the life of the Apache. It provides performance improvements that help the pilot track targets more effectively and mitigate the effects of aircraft vibration on the M-TADS/PNVS system.
The Apache has four articulating weapons pylons, two on either side of the aircraft, on which weapons or external fuel tanks can be mounted. The aircraft has a LRF/D. This is used to designate for the Hellfire missile system as well as provide range to target information for the fire control computer’s calculations of ballistic solutions.
LONGBOW FCR
The LONGBOW FCR has a very low probability of intercept. It rapidly and automatically searches, detects, locates, classifies, and prioritizes multiple moving and stationary targets on land, water and in the air in all weather and battlefield conditions from standoff ranges. Target coordinates are automatically available to other sensors and weapons for target confirmation, rapid engagement, and reduced fratricide. Target data is digitally available through the data modem for real-time transfer to other platforms and command posts. The self-contained Radar Frequency Interferometer provides rapid and accurate identification and azimuth to enemy air defense units. High system reliability and two-level maintenance maximize operational availability and reduce support costs. Source lockheedmartin.com
Image – globalsecurity.org
The Apache fully exploits the vertical dimension of the battlefield. Aggressive terrain flight techniques allow the commander to rapidly place the ATKHB at the decisive place at the optimum time. Typically, the area of operations for Apache is the entire corps or divisional sector. Attack helicopters move across the battlefield at speeds in excess of 3 kilometers per minute. Typical planning airspeeds are 100 to 120 knots during daylight and 80 to 100 knots at night. Speeds during marginal weather are reduced commensurate with prevailing conditions. The Apache can attack targets up to 150 km across the FLOT. If greater depth is required, the addition of ERFS tanks can further extend the AH-64’s range with a corresponding reduction in Hellfire missile carrying capacity (four fewer Hellfire missiles for each ERFS tank installed).
Army’s multidomain battle brings manned-unmanned teaming to the fore:Here
Excerpt
As the Army continues to develop its multidomain battle concept, manned-unmanned teaming will play a large role in operations going forward.
Despite multidomain battle being a new, updated vision to how the Army fights conflicts, the service has been conducting manned-unmanned teaming, or MUM-T, for some time, most notably involving Apache attack helicopter pilots being able to control MQ-1C Gray Eagles.
MQ-1C Gray Eagle
The MQ-1C Gray Eagle is powered by a single Thielert 2.0L heavy-fuel piston engine with 165 hp and provides an unmanned long-endurance and persistent ISR and tactical strike capability. The MQ-1C performs the following missions: Reconnaissance, Surveillance, Target Acquisition (RSTA), command and control, communications relay, signals intelligence (SIGINT), battle damage assessment, and manned-unmanned teaming capability. The Gray Eagle has a wingspan of 56 feet, is 28 feet long, and carries a payload of up to 1,075 pounds. The Gray Eagle is equipped with the Raytheon AN/AAS-53 Common Sensor Payload (CSP), which includes Electro-Optical/Infrared (EO/IR) video cameras and laser designators. The MQ-1C also features a Synthetic Aperture Radar (SAR), communications relay, and carries up to four AGM-114 Hellfire missiles. Source: fi-aeroweb.com
MIL-SPEC: Gray Eagle Manufacturer: General Atomics Aeronautical Systems (GA-ASI) Max. altitude: 29,000 feet Max. endurance: More than 30 hours Max. air speed: 135 knots true airspeed (approximately 155 mph) Payload: 1,075 pounds Engine: Thielert Centurion inline-four piston turbodiesel Displacement: 2.0L (121.5 ci) Bore: 3.26 inches (83 mm) Stroke: 3.62 inches (92 mm) Compression: 18:1 Dimensions (WxLxH): 30.63 x 32.12 x 25.04 inches (778 x 816 x 636 mm)
Manned-Unmanned Teaming Extended Capability (MUMT-X) provides the attack helicopter community greater situational awareness, real time battlefield video, and a common shared picture with troops on the ground. This capability increases an Apache crew’s coordination with other aircraft and Soldiers they support in battle. Apache is the first helicopter to utilize this technology./L-3 COMMUNICATIONS GRAPHIC
US Army sign $3.4 billion contract to acquire latest Apache attack helicopter with Manned / Unmanned Teaming:Here
Excerpt
Boeing and the U.S. government recently signed a five-year, $3.4 billion contract through which the Army, and a customer outside the U.S., will acquire the latest Apache attack helicopter at a significant savings to taxpayers. This is the first multi-year agreement for the Apache “E” variant. The Army will receive 244 remanufactured Apaches while 24 new ones will go to the international customer. More than 1,000 of the latest AH64-E model are expected to be produced for armed forces in the US, Europe and Commonwealth countries, as well as the Middle East and Asia.
AH-64 Apache helicopter gunships are flying night combat missions in support of the offensive to take the last major stronghold of the Islamic State in Iraq, a U.S. general said. “They’ve been flying at night, supporting any nighttime operations that the Iraqis are doing” since the Mosul offensive started Monday, Army Maj. Gen. Gary Volesky said of the Apaches in a video briefing from Baghdad to the Pentagon. “That platform has a lot of capability to see a long range at night and use its weapons system in a standoff capacity to strike targets, and that’s what they’re doing,” said Volesky, commander of Combined Joint Forces Land Component Command-Operation Inherent Resolve and the 101st Airborne Division (Air Assault).
The AH-64E is highly mobile, lethal and can destroy armor, personnel and material targets in an obscured battlefield conditions at ranges out to 8-kilometers, an Army statement said. The AH-64E is engineered such that aircraft can have the power, performance and landing abilities of earlier version with a much lighter weight making it more maneuverable and effective. It has a better engine that delivers 3,400 shaft horsepower compared to its predecessor’s 2,854. It has a new gearbox, an improved drive system and is lighter on fuel, meaning it can go further as well as faster.The AH-64E Apache is also 20 knots faster than the previous model and can reach speeds of 164 knots.
US Army RDECOM – AH-64E Apache Guardian Attack Helicopter Technology Upgrades & Improvements
Length: 58.17 ft (17.73 m) (with both rotors turning)
Rotor diameter: 48 ft 0 in (14.63 m)
Height: 12.7 ft (3.87 m)
Disc area: 1,809.5 ft² (168.11 m²)
Empty weight: 11,387 lb (5,165 kg)
Loaded weight: 17,650 lb (8,000 kg)
Max. takeoff weight: 23,000 lb (10,433 kg)
Powerplant: 2 × General Electric T700-GE-701 turboshafts, 1,690 shp (1,260 kW) [upgraded to T700-GE-701C (for AH-64A/D from 1990), 1,890 shp (1,409 kW)] each
Fuselage length: 49 ft 5 in (15.06 m)
Rotor systems: 4 blade main rotor, 4 blade tail rotor in non-orthogonal alignment
Performance
Never exceed speed: 197 knots (227 mph, 365 km/h)
Maximum speed: 158 knots (182 mph, 293 km/h)
Cruise speed: 143 knots (165 mph, 265 km/h)
Range: 257 nmi (295 mi, 476 km) with Longbow radar mast
1× 30 mm (1.18 in) M230 Chain Gun with 1,200 rounds as part of the Area Weapon Subsystem
The M230 is a single barrel, externally powered, electrically fired, chain driven weapon used on the Apache helicopters. It fires 30mm linkless ammunition.
Recent photos show the Israeli Air Force AH-64D carrying Rafael “Spike” missiles.
Taken by Noam Menashe recently, the images in this post show IAF AH-64D “Saraf” of the 113 “Hornet” Squadron based at Ramon, Israel, carrying the indigenous Spike missile system in what appear to be the NLOS (Non-Line Of Sight) variant.
According to AFM, the photos have been cleared by the Israel Defense Forces censor proving that the missile system is now officially considered part of the Israeli “Saraf” armoury.
The NLOS is an ultra-long range version of the precision attack system believed to have a maximum range of up to 25 km and a weight of 70 kg.
According to Rafael, the SPIKE NLOS weapon system can be operated in either direct attack upon target detection using LOBL (Lock-on Before Launch) Mode or firing from stand-off in automatic navigation mode based on operator or target acquisition system provided coordinates (INS navigation).
A bidirectional RF data link enables transmission of the missile seeker video image to the operator as well as real-time updating or steering of the missile.
Indeed, along with the range and non-line of sight firing capability, the electro-optically guided Spike has the ability to switch between targets and abort its mission if the operator believes the initial target should no longer be engaged.
ATAS to become a standard air-to-air component for Apache AH-64E: Here
Excerpt
Raytheon Missile Systems has entered a System Design and Development (SDD) contract with Boeing to integrate its FIM-92 Block 1 Air-to-Air Stinger (ATAS) missile as a standard air-to-air component for the E-model Apache AH-64 attack helicopter.
FIM-92A Stinger Weapons System
The Stinger system consists of a Stinger round encased in its launch tube and a separate gripstock assembly.
The “fire-and-forget” Stinger missile employs a passive infrared seeker to home in on its airborne target. A passive infrared seeker emits no radiation that a target aircraft can detect, and, instead, guides on the infrared energy (heat) emitted by the target. Because the Stinger employs a passive homing seeker, it is a “fire-and-forget” weapon that needs no guidance from the operator after firing, unlike other missiles that track the reflection of a designator beam, requiring the operator to maintain a lock on the target. This allows a Stinger operator to take cover, relocate, or engage other targets immediately after firing a Stinger.
The Stinger system features a proportional navigation system, integrated Indentification Friend or Foe (IFF) interrogation, and threat adaptive guidance. Proportional navigation enables the missile to effectively hit moving targets by injecting a multiplier factor into course corrections so that the missile overcorrects for a target’s evasive maneuvers, leading the target to a successful interception. The integrated IFF subsystem allows the Stinger operator to query a target aircraft to determine if it is friendly. Before firing, the operator depresses a button on the gripstock assembly, emitting a coded radio signal. Aircraft equipped with friendly IFF systems will recognize the coded signal and respond with the appropriate coded reply. The IFF subsystem emits one tone if it authenticates a friendly aircraft, and another if the aircraft is unknown. The IFF subsystem is intended to prevent friendly-fire incidents. The Stinger’s threat adaptive guidance takesover in the final stages of its approach to the target, slightly shifting the missile’s aim from the target’s IR hotspot to more vulnerable areas of the aircraft.
The Air-to-Air Stinger [ATAS] is an adaption of the man portable Stinger System. It is a light weight missile designed to engage low altitude targets.
Manufacturer
Prime – Hughes Missile System Company
Missile – General Dynamics /Raytheon Corporation
Propulsion
Dual thrust solid fuel rocket motor
Length
5 feet (1.5 meters)
Width
5.5 inches (13.96 centimeters)
Weight
12.5 pounds (5.68 kilograms)
Weight fully armed
34.5 pounds (15.66 kg)
Maximum system span
3.6 inches (9.14 cm)
Range
1 to 8 kilometers
Sight ring
10 mils
Fuzing
Penetration, impact, self destruct
Ceiling
10,000 feet (3.046 kilometers)
Speed
Supersonic in flight
USMC Units
Low-Altitude Air Defense (LAAD) Battalions: 3 active duty, 2 reserve
Crew
2 enlisted
Guidance system
Fire-and-forget passive infrared seeker
Warheads
High explosive
Rate of fire
1 missile every 3 to 7 seconds
Type of fire
“Fire-and-Forget”
Sensors
Passive infrared
Introduction date
1987
Data fas.org
Hydra 70 70 mm rockets and rocket pod
Hydra-70 Family
Image: defenceindustrydaily.com
In the following, the nine main variants of the Hydra-70 rocket are presented:
M151 High-Explosive:
The M151 HEPD is a unitary fragmenting 10-pound anti-personnel, anti-material warhead with the M423 Point Detonating Fuze. Upon detonation, the warhead fragments into thousands of small high velocity fragments. The fuzed warhead is 16.2″ long and weighs 9.3 pounds.
M156:
The M156 white phosphorus (smoke) is primarily used for target marking. The M156 has the same ballistic characteristics as the M151 warhead and is of similar construction. Filler for the M156 is 2.2 pounds of white phosphorus with a 0.12 pound bursting charge of composition B. The fuzed warhead is 16.2″ long and weighs 9.65 pounds.
M229 High Explosive:
The M229 High Explosive warhead is a heavier version of the M151. The U.S. Army is currently not buying this variant. The fuzed warhead is 26″ long and weighs 17 pounds.
M255A1 Flechette:
The M255A1 Flechette warhead consists of a nose cone assembly, a warhead case, an integral fuze, 1,179 60-grain flechettes and an expulsion charge assembly. The primary fuze (M439) is remotely set with the Aerial Rocket Control System (ARCS) Multifunctional Display (MFD) or Rocket Management System (RMS) to provide a range from 500 meters to 7,200 meters. At expulsion, the 1,179 60-grain, hardened-steel flechettes separate and form a disk-like mass which breaks up with each flechette assuming an independent trajectory. The flechette uses kinetic energy derived from the velocity of the rocket to produce the desired impact and penetration of the target. The fuzed warhead is 26.9″ long and weighs 14 pounds.
M257 Illuminating Flare:
The M257 Illuminating warhead is designed to provide battlefield illumination and does not require the use of Infrared (IR) goggles. The M257 flare rocket can be launched by from either fixed wing or rotary-wing aircraft. The M442 motor burnout fuze functions after a 9-second delay. The fuzed warhead is 29.1″ long and weighs 11 pounds.
M261 Multi-Purpose Submunition (MPSM):
The MPSM warhead (weight is 13.9 pounds) provides improved lethal effectiveness against area targets such as light armor, wheeled vehicles, materiel, and personnel. The M73 Submunitions are deployed over the target and descend almost vertically. The M261 Warhead is a cargo warhead consisting of a nose cone assembly, a case, integral fuze, nine submunitions, and an expulsion charge assembly. The primary M439 warhead fuze is remotely set with the Aerial Rocket Control System (ARCS), Multifunctional Display (MFD) or Rocket Management System (RMS) to provide a range from 500 meters to 7,200 meters.
M264 RP Smoke:
The M264 RP (red phosphorous) Smoke is used as a red phosphorous filled smoke rocket propelled by the Mk 66 motor and the smoke is deployed at a range set remotely from within the aircraft cockpit. The M264 warhead is used for smoke obscuration in the visible light spectrum. The fuzed warhead is 26.9″ long and weighs 8.6 pounds.
M274 Smoke Signature (practice):
The M274 warhead is a smoke/flash signature practice warhead used for pilot/gunner training missions and consists of a cast iron warhead modified with vent holes, an aluminum nose cap with firing pin, a M423 fuze safe and arming device, and a smoke/flash cartridge. The fuzed warhead is 16.2″ long and weighs 9.3 pounds.
M278 Infrared Flare:
The M278 Infrared Flare warhead is designed for battlefield illumination for use with Infrared (IR) goggles. The flare rockets can be launched from either fixed wing or rotary-wing aircraft. The 442 motor burnout fuze functions after a 9-second delay. The fuzed warhead is 29.1″ long and weighs 11 pounds.
WTU-1/B (practice):
The fuzed warhead is 16.2″ long and weighs 9.3 pounds.
Source fi-aeroweb.com
CRV7 70 mm short for “Canadian Rocket Vehicle 7”
CRV7 70 mm short for “Canadian Rocket Vehicle 7”, is a 2.75 inch (70 mm) folding-fin ground attack rocket produced by Bristol Aerospace in Winnipeg, Manitoba.
APKWS 70 mmair-to-ground rockets
AGM-114 Hellfire anti-tank missile
Primary Function: Air-to-surface and surface-to-surface point target/anti-armor missile Prime Contractor: Hellfire Systems, LLC – A Boeing – Lockheed Martin Joint Venture Propulsion:ATK (now Orbital ATK) solid propellant rocket motor (IM HELLFIRE Propulsion System);
AGM-114A: ATK M120E3; AGM-114B: ATK M120E4; AGM-114L: ATK M120E4 Length: 5.33 ft (1.62 m); AGM-114L: 5.77 ft (1.76 m) Diameter: 7 in (17.8 cm) Wingspan: 28 in (0.71 m) Weight: 98 to 109 lbs (44.5 to 49.4 kg); AGM-114R: 109 lbs (49.4 kg) Speed: Subsonic Range: AGM-114 K/L/M/N: 4.97 miles (8,000 m)
AGM-114R fired at 3,000 ft (914 m):
4.97 miles (8,000 m) – LOAL, high trajectory
4.41 miles (7,100 m) – LOAL, low/direct trajectory Guidance: Semi-Active Laser (SAL) seeker; AGM-114L: Millimeter wave (MMW) radar seeker Warhead: AGM-114 A/C/F/K/K-2/L/P/P+: Shaped charge warhead
AGM-114F-A/K-2A/P-2A: Shaped charge warhead with frag sleeve
AGM-114M/N: Blast fragmentation warhead (AGM-114N is a thermobaric version with metal augmentation charge)
AGM-114R: Multi-purpose Integrated Blast Frag Sleeve (IBFS) warhead
Source fi-aeroweb.com
MBDA Plans Brimstone 2 Missile Trial on AH-64 Apache:Here
Brimstone 2 precision attack missile
Brimstone 2 (SPEAR 2)
In March 2010 Brimstone was selected as the basis for the RAF’s requirement under the Selective Precision Effects At Range (SPEAR) Capability 2 Block 1 programme. The Demonstration and Manufacture (D&M) contract will increase the missile’s performance “significantly”, and convert the warhead and rocket motor to use insensitive munitions. Brimstone 2 will have an improved seeker, a more modular design and improvements to airframe and software for “an overall increase in performance with improvements in range and engagement footprint”, including a “more than 200% increase” in maximum range. A five-release test campaign in October 2013 culminated in a successful strike against a pickup truck travelling at 70 mph (110 km/h) in a cluttered road environment and Brimstone 2 is planned to enter service on the Tornado in November 2015.
Brimstone I:
20+ km (12+ mi) from fixed wing, 12 km (7.5 mi) from rotor wingBrimstone II:
60+ km (37+ mi) from fixed wing, 40+ km (25+ mi) from rotor wing
From the book of A. Mazepov, A. Mihkaev, V. Zenkin, A Zhirnov and A. Fomin about the Ka-50 called Polygon from 1996, on Page 31, there is said how the Armor was made on Ka-50 and after that also installed on Mi-28. It is a 3 hardlinered armor, the inner cockpit section made of a full single titanium alloy “bathtub” covering both pilots, followed by a middle liner of ceramic plates, which caused trouble first after a single shot they break apart and lost all its protective abilities, they avoided that by covering this ceramic plates with kevlar/aramid that was glued on tightend and the outer liner which gives the aerodynamic shape and is made of alluminium alloy with a part carbon in it. The total armor per pilot for russian Ka-50 which they could use was about 300kg while the Apache uses about 90kg of armor per pilot. The Mi-28 has about 250-280kg which was mentioned somewhere else. The Ka-52 has less armor than both Mi-28 and Ka-50 spend for each pilot but it is still in the figure of 150-200kg. (Source:Russian Defense)
120mm Compact L44 by RUAG
Image @media.defenceindustrydaily.com
Image – globalsecurity.org
1× 30 mm (1.18 in) M230 Chain Gun with 1,200 rounds as part of the Area Weapon Subsystem
Image: defenceindustrydaily.com
Thai Military and Asian Region 