bhagat
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Hindustan Aeronautics Limited is in the process of development of developing a Light Utility Helicopter (LUH). The LUH is a single engine helicopter in the 3000 Kg class. It is powered by a single turbo shaft engine with a dual channel FADEC and a backup fuel control. The helicopter will have a 3 axis AFCS. Cockpit is expected to include Smart Cockpit Display System Line replaceable Units (SCDS LRUs).
The LUH features a skid landing gear. Its spacious cabin is designed to accommodate six (6) passenger seats or four (4) VIP seats.
The helicopter will be capable of operating in all weather conditions. It will be cleared for both VFR and IFR day and night operations. The cockpit will be compatible with operation with Gen 3 and Gen 2++ NVGs.
It is planned to have both military and civil versions of LUH. The helicopter certification will be primarily based on FAR 27. However individual systems shall also comply with relevant military standards.
The military roles to be performed by LUH are primarily Utility roles with future variants for armed roles. The utility roles include Armed Reconnaissance, Aerial photography, Scout Role in conjunction with attack helicopter, Platform for Electronic Support Measure (ESM), Electronic Counter Measures (ECM) and Electronic Counter Counter Measures (ECCM).
LUH will be initially integrated with systems and equipment required for basic and military utility roles. Subsequently integration and certification of the helicopter for armed roles as well as civil / commercial variant would be taken up.
The Military variants of the helicopter would be certified by the Indian Military Airworthiness Certification agency CEMILAC.
The Civil variant of the helicopter is intended to be certified in India by DGCA and internationally through agencies like FAA, EASA.
LUH basic avionic systems inclide V/UHF Communication System(1st set), Intercom System, Radio Altimeter, Emergency Locator Transmitter (ELT), Global Positioning System (GPS)/ Global Navigation Satellite System (GLONASS)/ GALILEO, Flight Data Recorder (FDR), Cockpit Voice Recorder (CVR), Attitude and Heading Reference System (AHRS) and Air Data Unit (ADU).
Mission and role equipment include V/UHF communication system (2nd set), HF (SSB), Inertial Navigation System (INS) linked to GPS, VHF Omni Range (VOR)/ Instrument Landing System (ILS), Tactical Air Navigation System (TACAN), Digital Moving Map (DMM), Automatic Flight Control System (AFCS) and HMD with binocular display.
Weapon system and Mission sensors include Nuclear, Biological and Chemical sensors, Electro Optical System (EO), Fixed Sight and Flare & Chaff Dispenser (FCD).
Weapon Systems include Podded Gun, Rockets and Anti Tank Guided Missile.
Growth Potential Systems include Identification of Friend or Foe (IFF), Ground Proximity Warning system (GPWS), Digital Video Recording System (DVRS), Air-to-Air missile, Data Link, Obstacle Avoidance System (OAS), Radar Warning Receiver (RWR), Missile Warning Receiver (MWR), Laser Warning Receiver (LWR) and Weather RADAR
The LUH features a skid landing gear. Its spacious cabin is designed to accommodate six (6) passenger seats or four (4) VIP seats.
The helicopter will be capable of operating in all weather conditions. It will be cleared for both VFR and IFR day and night operations. The cockpit will be compatible with operation with Gen 3 and Gen 2++ NVGs.
It is planned to have both military and civil versions of LUH. The helicopter certification will be primarily based on FAR 27. However individual systems shall also comply with relevant military standards.
The military roles to be performed by LUH are primarily Utility roles with future variants for armed roles. The utility roles include Armed Reconnaissance, Aerial photography, Scout Role in conjunction with attack helicopter, Platform for Electronic Support Measure (ESM), Electronic Counter Measures (ECM) and Electronic Counter Counter Measures (ECCM).
LUH will be initially integrated with systems and equipment required for basic and military utility roles. Subsequently integration and certification of the helicopter for armed roles as well as civil / commercial variant would be taken up.
The Military variants of the helicopter would be certified by the Indian Military Airworthiness Certification agency CEMILAC.
The Civil variant of the helicopter is intended to be certified in India by DGCA and internationally through agencies like FAA, EASA.
LUH basic avionic systems inclide V/UHF Communication System(1st set), Intercom System, Radio Altimeter, Emergency Locator Transmitter (ELT), Global Positioning System (GPS)/ Global Navigation Satellite System (GLONASS)/ GALILEO, Flight Data Recorder (FDR), Cockpit Voice Recorder (CVR), Attitude and Heading Reference System (AHRS) and Air Data Unit (ADU).
Mission and role equipment include V/UHF communication system (2nd set), HF (SSB), Inertial Navigation System (INS) linked to GPS, VHF Omni Range (VOR)/ Instrument Landing System (ILS), Tactical Air Navigation System (TACAN), Digital Moving Map (DMM), Automatic Flight Control System (AFCS) and HMD with binocular display.
Weapon system and Mission sensors include Nuclear, Biological and Chemical sensors, Electro Optical System (EO), Fixed Sight and Flare & Chaff Dispenser (FCD).
Weapon Systems include Podded Gun, Rockets and Anti Tank Guided Missile.
Growth Potential Systems include Identification of Friend or Foe (IFF), Ground Proximity Warning system (GPWS), Digital Video Recording System (DVRS), Air-to-Air missile, Data Link, Obstacle Avoidance System (OAS), Radar Warning Receiver (RWR), Missile Warning Receiver (MWR), Laser Warning Receiver (LWR) and Weather RADAR