Daily Archives: July 15, 2016

SOM Air-to-Surface Cruise Missile

Stand-Off Missile (SOM) is Turkey’s first indigenous long-range, autonomous, high-precision air-to-surface cruise missile. It was designed and developed jointly by TUBITAK Defense Industries Research and Development Institute (TUBITAK SAGE) and Roketsan to defend ground- and sea-based targets.

The missile is highly effective against moving land / surface targets, high-value stationary targets, strategic assets, shelters, exposed aircraft, aircraft hangars, and command and control centres, as well as sea surface threats. It has resistance against countermeasures as well as clutter effects.

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SOM – savunmasanayist.com

In October 2014, Roketsan and Lockheed Martin Missiles and Fire Control signed a teaming agreement on the development of a new generation stand-off cruise missile variant, SOM-J for internal carriage on the F-35 Lightning II fifth generation multi-role stealth fighter or external carriage on other aircraft.

“Lockheed Martin has a long history of partnership with the Republic of Turkey and we look forward to working closely with Roketsan on this very important project,” Edwards said. “SOM-J will provide the F-35 and other aircraft an exceptional capability to meet the most challenging mission requirements. We look forward to combining the skills and know-how of our two great companies to produce a world-class system to meet customers‘ expanding needs for long-range, survivable cruise missile technology.” Source roketsan.com.tr

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ssb.gov.tr

The Stand-Off missile was exhibited at the International Defence Exhibition & Conference (IDEX) 2015 held in Abu Dhabi, UAE.

Development of Turkey’s first indigenous stand-off missile

Development of the SOM cruise missile began in 2006. The missile was unveiled at the 2nd Air Force Base located in Çiğli, İzmir in June 2011. It has been in service with the Turkish Air Force since 2012 and is certified for integration onto the F-4E 2020 and F-16 Block 40 fighter aircraft.

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gaste24.com

It was first test-fired from a McDonnell Douglas F-4E 2020 strike aircraft in August 2011.

The Undersecretariat for Defense Industries under the Ministry of National Defense placed a $25m worth contract with Kale Aero in February 2012 to develop turbojet engines for the SOM weapon system.

Design and features of SOM cruise missile

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Som – instagramwebs.com

The SOM cruise missile features a modular design, offers high-lethality and delivers enhanced operational flexibility. It has a low detectable capability and a longer range compared to surface-to-air missiles. It is compatible with the Nato UAI standard.

The missile is capable of performing in-flight re-targeting as well as in-flight mission selection among pre-planned missions. Its rear section is fitted with control fins for providing lifting and improved manoeuvrability.

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sage.tubitak.gov.tr

Suspension lugs fitted to the missile provide mechanical interface between the missile and the launch aircraft. The weapon system also incorporates a power system, fuel tank, air inlet, wing deployment system, and a missile computer.

The missile system weighs 600kg and is equipped with a 230kg blast fragmentation and dual stage tandem penetration warhead. It features selectable impact parameters.

Operational Characteristics

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  • Long Range (250+ km)
  • Low Observable
  • High Precision Navigation with INS/GPS/TRN/IBN
  • High Precision Terminal Guidance with IIR and Data Fusion
  • Resistance to Counter Measures / Clutter
  • Wide Firing Envelope Allows Off-Boresight Engagement
  • Target of Opportunity Capability
  • In Flight Mission Selection
  • In Flight Retargeting
  • Selectable Impact Parameters
  • NATO UAI Compatibility
SOM-A SOM-B1 SOM-B2
Length ~4 m ~4 m ~4 m
Weight 1300-lb Class 1300-lb Class 1300-lb Class
Range 250+ km 250+ km 250+ km
Warhead ~500-lb High Explosive / Blast Fragmentation ~500-lb High Explosive / Blast Fragmentation ~500-lb High Explosive / Blast Fragmentation
Seeker Imaging Infrared Imaging Infrared
Guidance Systems INS/GPS/TRN INS/GPS /TRN/IBN/ATA INS/GPS /TRN/IBN/ATA
Platforms F-4
F-16
F-4
F-16
F-4
F-16

Source roketsan.com.tr

Guidance and navigation

SOM is equipped with an imaging infrared (IIR) seeker and an inertial measurement unit (IMU) for high-precision guidance. The IIR seeker incorporates a high-resolution imaging system and allows detection of predefined targets with long ranges, high-agility, and resistance to electronic countermeasures / clutter.

The cruise missile is navigated using global positioning system (GPS), inertial navigation system (INS), terrain referenced navigation (TRN), image-based navigation (IBN), and automatic target recognition (ATR) sensors. It also incorporates a radar and barometric altimeter for determining the flight altitude, and has the ability to follow waypoints and terrain contours.

Propulsion and performance of SOM missile

The Stand-Off missile is powered by a turbojet engine and has a range of more than 180km. It is operable under all weather conditions, and also in hostile environments.

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lockheedmartin.com

Engine

KTJ-3200 Turbojet engine developed by Kale Arge to be used in SOM Cruising Missile and the sub-systems of the engine have started the qualification tests. Upon completion of the qualification tests, acceptance tests of the KTJ-3200 will begin. If the tests are successful, the KTJ-3200, which is planned to become operational in 2019, will end the bağımlılık critical dependency indeki in the SOM project. In addition, the engine can be used in various projects with various modifications.

SOM Missile developed by TÜBİTAK-SAGE and produced by Roketsan in series production. Within the scope of the Motor Engine Development Project K, the KTJ-3200 turbojet engine, which was started to be developed by Kale Arge in 2013, will replace the TR-40 Turbojet Engine, which is currently used in the serial production of the SOM Missile and supplied from France. In addition, thanks to the domestic engine SOM Missile, range can be increased. Translated by google source savunmasanayist.com

Microturbo TRI 40

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TRI 40 – The latest addition to the Microturbo engine family. The small size and high thrust-to-weight ratio make the TRI 40 a promising propulsion unit for state-of-the-art anti-aircraft missiles, training targets and unmanned aircraft. The engine has a four-stage compressor and a single-stage turbine, working on fuel JP8 and JP10. Depending on the version, the engine thrust ranges from 250 to 340 kg. Optimal conditions for engine operation are set at a flight altitude of 0-6000 meters and a maximum speed of M = 0.95. It can be started at speeds M = 0.5 to M = 0.9 at altitudes up to 5300 meters. The first “flying vehicle” with the engine TRI 40 is an anti-missile missile NSM company Kongsberg Defense & Aerospace and MBAD. Source leteckemotory.cz

KTJ-3200 Turbojet engine

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Our turbojet engine, the KTJ-3200, was developed specifically for the navigation missiles, as well as target aircraft, etc. is a Turbojet Engine optimized for use on unmanned platforms.

Its compact design has high propulsion, low fuel consumption and can be started at different altitude / speed conditions.

Turkey’s first national turbojet engine that has KTJ-3200 feature, altitude using our test system, different altitude / performance in terms of speed has already been shown by the year 2019. However; strength, water uptake, degradation, environmental tests are passed through many different tests. All the tests are carried out in Turkey.

In 2019, the qualification of our KTJ-3200 engine will be completed.

Thanks to its superior features, the KTJ-3200 can be quickly adapted to different domestic and foreign platforms with modifications to be made to the needs. Source airturkhaber.com

Details of the SOM-J variant

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SOM-J – lockheedmartin.com

The advanced SOM-J variant will be jointly developed, produced, marketed, and sold by Lockheed Martin and Roketsan. The first stage of SOM-J is scheduled for completion in 2018.

The variant is intended to provide exceptional anti-surface warfare capabilities to the F-35 Lightning II Joint Strike Fighter and other similar aircraft.

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SOM-J – lockheedmartin.com

Main Features

  • Long Range (120+ NM)
  • Low Observable
  • Highly Survivable
  • High Precision Navigation with INS/GPS/TRN/IBN
  • Highly Precise Terminal Guidance with IIR and Data Fusion
  • Target of Opportunity Capability
  • In-Flight Retargeting
  • Network Enabled Weapon (NEW) Capability
  • Universal Armament Interface (UAI) Compatibility
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SOM-J – lockheedmartin.com

Technical Specifications

Length ~4 meters
Weight 1000-lb Class
Range 120+ NM
Warhead ~310-lb Blast Fragmentation / Semi-Armor Piercing
Seeker Imaging Infrared
Guidance System INS / GPS / TRN / IBN / ATA
Platform F-35 / F-16

Source roketsan.com.tr

Main material source airforce-technology.com

Images are from public domain unless otherwise stated

Revised Aug 04, 2019

Safran Helicopter Engines to form Indian JV with HAL

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12 Jul, 16, Source: Safran

Safran Helicopter Engines and Hindustan Aeronautics Ltd. (HAL) have agreed to establish, in India, a support centre for national and international rotorcraft customers. The joint venture will be opened in the coming months.

This new centre will provide maintenance repair and overhaul (MRO) services for Safran TM333 and HAL Shakti engines installed on HAL-built helicopters. This scope would be enlarged to include other engines which both partners may further agree. Safran Helicopter Engines and HAL will provide their customers with a first-class service including optimized engine availability.

With a fleet of over 1,000 engines, including 250 TM333 and 250 Shakti, India’s armed forces are one of the largest operators of Safran-designed helicopter engines. Shakti is the Indian designation for the Safran Ardiden 1H1, co-developed with HAL and produced under license.

T. Suvarna Raju, HAL Chairman and Managing Director said: “The venture reflects the close relationship established over many years between HAL and Safran Helicopter Engines. It places both partners on an ambitious path towards world-beating customer support in the field of engine MRO”.

Bruno Even, Safran Helicopter Engines CEO, commented “this joint venture marks a new step in the long-lasting and fruitful partnership between Safran Helicopter Engines and HAL. We are extremely proud of the continued confidence placed in us by HAL. Together we are committed to delivering world-class support to our customers, both in India and throughout the region”.

The joint venture will provide the impetus for the “Made-in-India” initiative and its ambition of flying around 1,000 Shakti engines in India during the coming years.
Shakti is fitted to HAL’s ALH/Dhruv and has been selected to power the HAL-designed Light Combat Helicopter (LCH). Ardiden 1U variant powers the new Light Utility Helicopter (LUH), a three-ton single-engine aircraft under development.

Original article @helihub.com

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TM 333

Ardiden1H1__SafranHelicopterEngines_RemyBertrand.578500d7d5d8b

The engines of the TM 333 family cover a power range from 900 to 1100 shp. They are intended for helicopters 3 to 6 tons.

The TM 333 powers the Dhruv twin-engine helicopter of Hindustan Aeronautics Limited (HAL). 300 TM 333 have been produced to date, with more than 65,400 flight hours.

The TM 333 was originally designed to power the twin-engine Dauphin and Panther Helicopters Airbus. Developed on the Panther, he found its first commercial application on the Dhruv.

The TM 333 adopts a simple architecture consists of two main modules which are: a compressor with two axial stages and one centrifugal stage, a combustion chamber in reverse flow, a gas generator turbine with a floor, and a turbine free power to a floor.

Source @safran-helicopter-engines.com

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Airbus Signs With Roketsan To Add Missiles, Bombs to C-295

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, Defense News10:01 a.m. EDT July 14, 2016

FARNBOROUGH, England — Airbus and Turkey’s Roketsan have signed to arm Airbus’ C-295 aircraft with laser-guided missiles and bombs, part of Airbus’ drive to give the widely sold transport plane new roles.

The two firms signed a memorandum of understanding at the Farnborough International Airshow on Wednesday to team on the design, integration and testing of Roketsan weapons, including the 70mm laser-guided Cirit missile and the long-range, laser-guided L-UMTAS anti-tank missile, as well as the Teber laser-guided bomb.

“There is a clear opportunity for us to address the global requirement for a cost-effective, armed utility aircraft, and Roketsan’s product range and proven expertise make them the obvious partner,” said Airbus’ head of military aircraft, Fernando Alonso.

The move forms part of Airbus’ expansion program for the C-295, which is already used as a maritime patrol aircraft by four customers.

The next step is to introduce an electronic intelligence and communications intelligence version, as well as an aircraft with early-warning capabilities, said Fernando Ciria, Airbus’ head of marketing for tactical airlifters and ISR.

Also on the list is a ground surveillance version for border control missions, with a radar offering ground moving target indicator and synthetic aperture radar functions yet to be selected, said Ciria.

“Some customers are also interested in strike capabilities,” he said, adding that pylons now fitted for torpedoes on the maritime patrol versions would be used for the Roketsan munitions, with target designators also added.

To date, Airbus C-235 aircraft obtained from the Spanish Air Force have been turned into gunships by ATK for use by Jordan.

As further evidence of its move to extend the use of the C-295, Airbus used the air show to show off an aircraft rigged to provide in-flight refueling to other slow-moving aircraft or helicopters.

The roll-on, roll-off system contains 90 feet of tubing and a refueling basket, which can be extended from the open ramp at the rear of the aircraft, with the capacity to provide 6 tons of fuel, said Ciria.

Read original post @defensenews.com

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C295 refueling capabilities

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Image @airbusgroup.com

2.75” Laser Guided Missile CİRİT

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Properties of the Product

CİRİT, is a missile with the longest range in its class which provides a superior precision against light, armored/unarmored and stationary/mobile targets as well as being a cost effective solution.

Basic Specifications

  • The 2.75″ Missile with the Longest Range
  • Insensitive Munitions (Level V)
  • Multi Purpose (Armor Piercing, Anti Personnel and Incendiary) Warhead
  • Integration to Various Platforms (Helicopter, UAV, Land Vehicle, Stationary Platform, Light Assault Aircraft, Naval Platform)
  • Standard Mode and Smart Mode Pod Integration
  • Not a Guidance Kit, New Generation All-Up Round Missile System
  • Composite Propellent Technology with Reduced Smoke

In the Inventory of Turkish Armed Forces

Cirit canister
Diameter 2.75″ (70 mm)
Maximum Range 8 km
Minimum Range 1,5 km
Weight 15 kg (Without tube complete)
Propellant Type HTPB Based, Smokeless, Composite Solid Propellant
Warhead Type Multi Purpose Warhead, Armor Piercing, Personnel, Incendiary
Warhead Type High Explosive Warhead
Guidance Mid – Phase Guidance with MEMS – AÖB
Guidance Terminal Guidance with Semi-Active Laser Seeker
Target Types Light Armored / Unarmored Vehicles, Stationary and Moving Targets, Bunkers
Platforms Helicopters (AH – 1W, T – 129 ATAK etc.), UAV’s,  Land Vehicles, Light Assault Aircraft, Naval Platforms and Stationary Platforms 

Data @roketsan.com.tr

L-UMTAS anti-tank missile

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Image @roketsan.com.tr

Properties of the Product

  • UMTAS, with its Imaging Infrared Seeker and Laser Seeker options, is an anti-tank missile, having a range of 8 km and lock on before/after launch and “fire and forget/fire and update” properties, used against armored targets, from air to ground as well as ground to ground.

Basic Properties

  • Insensitive Munitions (Level V)
  • Tandem Warhead Effective Against Reactive Armors
  • Integration to Various Platforms (helicopter, UAV, Land Vehicle, Stationary Platform, Light Attack Aircraft, Naval Platform)
  • IIR or Laser Seeker Options
  • Lock on Before / After – Launch
  • Fire and Forget / Fire and Update Properties
  • RF Data Link
  • Smokeless Composite Solid Propellant

Product Description

UMTAS, which was developed by Roketsan primary for use from attack helicopters, is an antitank missile system. With its advanced technology it is highly effective against all armored threats in the field.

UMTAS, with its maximum range of 8 km and minimum range of 500 m is capable of operating all weather conditions and day/night.

UMTAS, which can be used in Fire and Forget and Fire and Update modes, with the flexibility provided by its target update capability, offers to fire behind the mask position, fire against targets hiding behind mask and adjust hit point and damage assesment capability. UMTAS, defined as the official antitank system of the National Attack Helicopter (T – 129) under development, can be integrated to various platforms (Helicopter, UAV, Land Vehicle, Stationary Platform, Light Assault Aircraft, Naval Platform)

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Image @roketsan.com.tr

Technical Specifications

Diameter 160 mm
Max. Rangel 8 km
Min. Range 0,5 km
Weight 37,5 kg
Propellant Type HTPB-Based Reduced Smoke Composite Propellant
Warhead Type Insensitive Tandem Warhead Effective Against Armor with Reactive Protection
Guidance Imager Infrared (IIR) or Laser
Target Types Heavy Armored / Armored Vehicles
Platforms Helicopters (AH – 1 W, T – 129 ATAK etc.), UAV’s,  Land Vehicles, Light Attack Aircraft, Naval Platforms and Stationary Platforms

Source @roketsan.com.tr

Teber laser-guided bomb

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TEBER system is designed to increase the probability of hit, against moving target. TEBER is compatible with Mk-81 and Mk-82 general purpose bombs.
TEBER consists of a semi-active laser seeker (SAL), a (body) strake kit that is located in the front section. Tail section has aerodynamic control surfaces, inertial guidance system combined with GPS/GNSS receiver, guidance computer, control actuation system and thermal battery.
Growing interest for TEBER for the requirements of Gulf countries is expected.

Guidance Modes INS onlyINS+GPS

INS + GPS + Laser

Range 2 – 8 Nautical Mile (Depending on release altitude)
CEP – 50 < 3 m
Maneuver Capability ± 3 g
Moving Target Engagement Up to 110 km/s
Weight  (Mk-82, Mk-81) ~270 kg (595 lb), ~155 kg (345 lb)
Length  (Mk-82,Mk-81) 2650 mm (104’’), 2100 mm (81.5’’)

Source @mea-aviation.com

MC-27J ATK: Details

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Argentine electronic warfare aircraft breaks cover

14 July 2016

Pictures of the Argentine Air Force’s Learjet 35A were released earlier this month, depicting an aircraft modified specifically for countering electronic warfare.

Argentina has not has such an aircraft since retiring the Boeing 707 VR-21.

The Air Force acquired the 35A in 2013 and contracted Avcon Industries to make the necessary modifications to allow installation of a Thales Vigile 200 electronic support system.

Other modifications include tanks on the wingtips so antennas could be fitted, compartments and new wiring for antennas, a radome on the tail, and structural changes for delta wings to achieve better stability and efficiency.

Original post janes.com

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Argentine Air Force’s Learjet 35A

t-22-fuerza-area-argentina-learjet-35a_PlanespottersNet_361878Buenos Aires – Aeroparque Jorge Newbery (AEP / SABE), Argentina 03 February, 2013 Image @planespotters.net

Installation of a Thales Vigile 200 electronic support system

12/02/2014 (Infodefensa.com) Montevideo -. Through direct purchase by Speciality No. 58 of 2014, the Argentina Air Force has hired the company Avcon Industries Inc. to undertake the necessary structural modifications that allow installation in the Learjet 35A enrollment

vigile_200_02

VR-24, an ESM Thales Monitor 200 system, which was acquired earlier. The tasks to be accomplished in Argentina, include modification and installation of the tanks of the wingtips creating watertight compartments for antennas, a radome of tail, wiring from antennas to the warehouse where the equipment data processing are, relocation of antennas that can hinder new equipment and structural modifications / facilities necessary for adapting Delta Fins, to improve stability and efficiency of the aircraft. the Thales Monitor 200 is a RESM system (Radar Electronic Support Measures) detection usually installed on naval platforms for detection radars operating between 0.5 and 18 GHz with a 360 – degree coverage. gp / CEH Photo: Thales. Source tecnologiabelicayarmas.blogspot.com

23388415419_a320671c79_bImage @Javier Parigini Bombardier Learjet LJ-35A | by ..Javier Parigini