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ALAS (missile)

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Attack system). RALAS has a 10.5 kg tandem warhead capable to penetrate over 1,000 mm RHA, or a blast fragmentation one with a 25 meters lethal radius. RALAS is intended for use from land or helicopter platforms for launch. RALAS(LORANA) missile seeker was tested in mid 2012 on light aircraft SILA 450C domestic aircraft (made in Kraljevo, Serbia by Aero-East-Europe) in a series of 10 flights above "Pasuljanske livade" military multibranch exercise range. RALAS is an advanced remote non-line of sight attack system battery that consists of a battery command post (based on light wheeled armored SUV or semi) and four launch vehicles, with each vehicle equipped with 4 to 8 containers with missiles. A missile carrier is available for reloading missiles or as a backup control car.
544: 558: 54: 528: 284: 32: 180:. The ALAS missile system was developed primarily for missions against tanks, armored vehicles, fortifications, command posts, low-flying helicopters, coastal ships, industrial facilities and bridges. It can be deployed by any suitable platform including helicopters, armored vehicles, small ships and infantry. The guidance system is based on video/ 369:
north-seeking device. The firing station is used for mission planning before the engagement. The firing station stores a digitized map and displays the map during missile flight. For some applications, a dual monitor system is used. The firing unit can be used as a trainer and simulator without additional hardware.
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The nose missile is mounted with a video unit that allows target detection the size of a tank at distances of 3 km. The field of view available on the display unit is 7 ° x 5 °. The fiber optic cable can handle pulling forces of 52 N. Loss of signal in an optical cable is 0.2 dB / km. The
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6x6 chassis. The ALAS-C abandoned the initial design and moved the arrow wing forward. It used a small degree of aerodynamic control via rudders and was propelled by an axial turbine engine equipped with a single nozzle. ALAS-C missiles installed the turbojet in the stretch LORANA of missile X-type
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RALAS (Rocketized Alas) has solid propellant sustainer rocket engine, accelerated with solid propellant booster engine variant can replace the turbojet with range estimated to 9–10 km with greater speed. It was in early stages of development designated as LORANA (LOng RAnge Non line of sight
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Another possible application of the ALAS missile system would be to defend an airfield and conduct surgical strikes until heavier forces are available. Its range could extend the close-combat kill zone to 5–25 km in front of the forward line of its own troops and for deeper strikes up to
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Firing station comprises a high-performance compact computer for missile guidance, an operator control panel and a high-resolution display. The system uses advanced control and image processing algorithms, electro-optical converters and radio links. The firing station has an optional GPS and
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During launch, a solid propellant booster accelerates the missile to an initial cruising speed (120–150 m/s). Then the TMM-040 turbojet ignites to take the missile to the target under control of the guidance system and the operator. Main propulsion characteristics:
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cable provides an on-board missile data transmission rate of 128 kbit/s and from the missile to ground control data transmission speed of 240 Mbi /s - available on one video channel and two data channels.
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Solid propellant booster is positioned on the rear side on the missile body placed after turbojet engine with requirements that thrust vector direction going through missile center of gravity position.
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The ALAS missile is hot-launched from its canister by means of a solid-propellant boost motor. ALAS is the designation for missiles produced in ALAS-A, ALAS-B and ALAS-C variants.
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Communication subsystem based on fiber optic cable connection to transfer real-time (part of communication sub system are roll with fiber optic cable with a length of 9 km)
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The operative flight envelope (required for flight and control system) in the radial axis with respect to the axis of motion is ±3 g, whereas in the axial direction it is 10 g.
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RALAS(LORANA) can be stored in a container more than 10 years without maintenance. After the installation on the carrier the rocket is ready for immediate use.
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The missile is programmed to follow a preset course around or over any obstructing terrain using electronic terrain maps. The terminal guidance phase uses an
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guidance system, the ALAS-C will have a range of up to 25 km, using a video/CCS/IIR system to deliver its fragmentation warhead.
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Group fired solid fuel propellant formed starting rocket engine and flight rocket engine (both engines developed by EDePro company)
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Missile main engine is a Mongoose 040 turbojet that permits a sub-sonic top speed of around 640–740 km/h (340-400 mph).
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Subsystem management and control: warhead anti-tank tandem with 1 meter penetration of rolled, homogeneous armor steel
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Guidance head with a gyro-stabilized TV camera or Infrared seeker that uses either a contrast or a correlation algorithm
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Striking land-based targets from the sea. In this scenario, the missile is launched from a small ship or a helicopter.
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The rocket engine uses two laterally inclined nozzles with 300 N thrust and maximum specific impulse of 14 000 N
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long-range multipurpose wire guided missile system developed by the private company EdePro and the state-owned
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Missile communication is realized via optical monomode cable with two channels (communication directions):
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The firing station works similarly to ALAS. RALAS(LORANA) can achieve a maximum deviation of 1 m.
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solid fueled boost phase motor, EdePro TMM-404 single-shaft turbojet ALAS, rocket engine RALAS
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image making it possible to transfer thermal images back to the launching platform via a 200
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contains two, flat, engine nozzles and a fiber spool. Employing an INS or optionally a
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ALAS-C (Coastal Defence) is an anti-ship variant that is in mutual development between
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Electronic transmission apparatus for laser video signal to digital signal receiver
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On order first patch of 60 missiles in 2023–2024. Launching platform is M18 Oganj.
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The two main types of system depend on missiles used as ALAS or RALAS system.
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When attacking ships, missiles can fly at an altitude of a few meters above
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Striking isolated targets from light land vehicles and for anti-ship combat.
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Defence Technology Analysis Department: ฝ่ายวิเคราะห์เทคโนโลยีป้องกันประเทศ
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The ALAS missile system is intended to attack distant targets, such as:
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RALAS missile consists of the following functional units/sub-systems:
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ALAS-B is a surface to surface variant with a range of 60 km.
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ALAS-A is a surface to surface variant with a range of 25 km.
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The ALAS missile system is intended for two primary missions:
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technology, with the missile connected to the launcher by a
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RALAS is planned to be integrated on two mobile platforms:
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with 25 km or 50 km range in future development.
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For the United Arab Emirates it will be delivered on the
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Missile takes off from the shipping container-starter.
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In launch phase uses two assigned propellant boosters.
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Image transmission and data from missile to ground.
364:Data transmission from ground station to vehicle. 203: 975: 867:"Lorana missile seeker tested on light aircraft" 714:"IHS Events, Webinars, Training and User Groups" 637:fiber optics guided multiple purpose missile 244:Small boats, ships and other coastal targets 822:"IDEX 2019: Yugoimport, from ALAS to RALAS" 241:Hardened targets larger than 5 by 5 meters 31: 697: 526: 282: 864: 976: 865:Gyürösi, Miroslav (October 30, 2012). 683:: CS1 maint: archived copy as title ( 456:Missile flight speed: 120–200 m/s 287:ALAS guided missile launch vehicle on 989:Surface-to-surface missiles of Serbia 894: 892: 890: 888: 613:XM501 non-line-of-sight launch system 506:ALAS is planned to be integrated on: 486: 736: 734: 535: 984:Anti-tank guided missiles of Serbia 13: 885: 475: 14: 1005: 731: 109:175 mm × 1,450 mm (wingspan) ALAS 16:Serbian long-range guided missile 556: 542: 428: 321:Speed: 180 m/s (mid-course) 226: 52: 941: 927: 913: 531:Map with ALAS operators in blue 164:(advanced light attack system, 43:Long-range multipurpose missile 858: 828: 814: 784: 752: 706: 691: 648: 204:Description of system and role 1: 642: 463: 379: 101:2700 mm ALAS-A, 1800 mm RALAS 900:"Srbská riadená strela ALAS" 765:. April 2013. Archived from 522: 449:Rocket motor thrust is 4500 446:Warhead weight: 10.5 kg 7: 570: 337: 248: 10: 1010: 453:: burn time is 3.5 seconds 350:data link provided by an 330:Penetration: 800 mm 315: 238:Tanks and combat vehicles 235:Static land installations 169: 148: 136: 126: 118: 113: 105: 97: 89: 84: 70: 65: 48:Place of origin 47: 39: 30: 23: 399: 443:Base weight: 60 kg 256: 630:France, Germany, Italy 577:AFT-10 Missile Carrier 532: 292: 530: 437:Diameter: 175 mm 286: 824:. February 23, 2019. 300:wing control of the 802:on February 6, 2015 772:on February 6, 2015 324:Altitude: 150–500 m 192:motor instead of a 994:Serbian inventions 533: 487:Launching platform 434:Length: 1.8 meters 293: 152:less than 1 meter 66:Production history 959:on March 27, 2013 748:on July 10, 2013. 665:on March 13, 2021 536:Current operators 327:Range: 25 km 186:fiber-optic cable 159: 158: 1001: 969: 968: 966: 964: 955:. 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Index


Serbia
EdePro
Yugoimport SDPR
CEP
Serbian
Serbian
Yugoimport SDPR
infrared
fiber-optic cable
turbofan
turbojet
UAV
Serbia
the UAE

Nimr
Nimr
rudder
elastomer
GPS
RHA
infrared
MBit/s
optical fibre
sea level
Newtons
Lazar 3
M18 Oganj
M18 Oganj

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