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HAL’s LCH (Light Combat Helicopter) Makes Its Maiden Flight

By Air Marshal B.K. Pandey (Retd), Bengaluru & Air Marshal V.K. Bhatia (Retd), Delhi

India’s aerospace industry crossed a significant milestone in its march towards self reliance when the first prototype of the five tonne class LCH, designed and developed by the Hindustan Aeronautics Ltd (HAL), was unveiled at Bangalore on May 23, 2010. Wing Commander Unni Pillai, the Chief Test Pilot of HAL, duly assisted by the co-pilot Group Captain Hari Nair, staged an impressive 20 minute aerial demonstration of this new highly manoeuvrable and versatile machine. The profile included the reverse slide which perhaps is one of the most difficult and tricky manoeuvres to perform.

The event was witnessed by Air Marshal P.K. Barbora, Vice Chief of Air Staff who was the Chief Guest, R.K. Singh, Secretary, Defence Production, several senior functionaries from the armed forces and the defence industries and research establishments. On account of the gruesome air tragedy at Mangalore the previous day which resulted in heavy loss of life, Defence Minister A.K. Antony, Minister of State for Defence Pallam Raju, and Chief of the Air Staff Air Chief Marshal P.V. Naik were unable to attend the ceremony.

Dedicating the LCH to the nation, Air Marshal Barbora, complimented the HAL for the successful design and development of the machine which he described as “no mean achievement”. He stated that the LCH is “badly needed” by the Indian Air Force and hoped that the machine would be ready to enter service in 2-3 years. He hoped that the overweight problem which is commonly encountered in the development of new aircraft would be corrected in due course before its operational induction into the IAF.

Addressing the gathering, R.K. Singh, Secretary, Defence Production, said that the LCH was a "truly fine" machine and that the indigenous development of the helicopter was important for both strategic and economic considerations. He was hopeful that the LCH would receive initial operational clearance (IOC) by the end of 2010 and final operational clearance (FOC) soon after. He stressed the vital need for India to achieve high levels of self reliance in the regime of defence production as also in respect of research and development capabilities.

“It is a red-letter day for not only Hindustan Aeronautics Limited (HAL), but the whole nation. I am quite positive that the aircraft will meet all Indian Air Force (IAF) requirements in this class of helicopters. The first flight has been superb,” said an enthused Air Marshal P.K. Barbora, the IAF’s Vice Chief of Air Staff after witnessing the maiden official flight of the indigenous Light Combat Aircraft (LCH) on May 23, at HAL’s Bangalore airport.

Flawless First Flight

It seemed a good effort by HAL to indigenously design, develop and test fly the LCH since the project began in full earnest in 2006 at a projected cost of 376 crore ($80 million). The idea of a light combat aircraft was conceptualised way back in 1989 by HAL based on an IAF requirement. However, it was just as well that the government clearance came only in 2006 by when HAL’s Advanced Light Helicopter (ALH) Dhruv had not only reached full maturity, but had also been inducted for operational service. The earlier design which had debuted in 2001 at the Paris Air Show as the Light Attack Helicopter (LAH) was heavily restyled into what came to be known as the LCH. A derivative of Dhruv, the original slimmed-down “gunship” fuselage was discarded and basic Dhruv airframe was retained except for forward fuselage which was modified to tandem crew seating. The LCH incorporates several features of the HAL built ALH Dhruv, which includes the hinge-less rotor, transmission system, Shakti engine, hydraulics, full glass cockpit, integrated defensive aids suite (IDA) and weapons systems.

Developed for dedicated combat role, the unique features that provide agility, survivability and lethality to the LCH are its narrow fuselage for low drag profile, armour protection of critical areas, crashworthy landing gear with a tail wheel, crashworthy and self sealing fuel tanks, aerofoil shaped stub wings for weapons, electronic warfare suite, self-protection suite (SPS) consisting of radar/laser missile warning systems and counter-measures dispensing system (CMDS), armour and NBC protection as also stealth features. It is also planned to integrate IR/laser missile jammer on the helicopter. The gear box has the capability of running for 30 minutes even after total loss of oil in case of a ballistic damage to the transmission system. Dual redundant systems also enhance survivability in a battlefield environment.

When fully developed, the armament suite of the LCH will comprise a 20 mm turret gun in the nose slaved to the helmet mounted sights of the Pilot and the Flight Gunner. The LCH will also carry rocket pods, air defence missiles and air-to-surface missiles on the weapon stations under the stub wings. It will be equipped with “target acquisition and designation system” providing day/night targeting capability through electro-optical pod consisting of CCD camera, FLIR, laser range finder and laser designator. A digital video recorder would enable recording of the entire mission for post mission debrief. Equipped with data link that would facilitate transfer of the mission data to the other airborne platforms and ground station, the helicopter would be capable of operating in a network-centric environment. (See box below for general/performance characteristics).

The performance of the LCH i.e. rate of climb, cruise speed, service ceiling, etc., are on a par and on some scores even better than other helicopters in its class like AW129 Mangusta or the Eurocopter Tiger, the helicopters it has great resemblance with. It may be recalled that for the eventual and inevitable phasing out of its ageing fleet of Mi-25/Mi-35 attack helicopters, the IAF had issued a RFP for the acquisition of 22 attack helicopters worth over $500 million (2,315 crore) in May 2008 to leading global manufacturers which included US Bell (AH-1Z Cobra) and Boeing (AH-64 Apache), British-Italian AgustaWestland (AW129 Mangusta), EADS Eurocopter (Tiger), Russian Mil (Mi-28) and Kamov (Ka-50/52). The RFP had later fallen through for a multitude of reasons with the responsibility for the same on the shoulders of many players. The RFP has since been reissued hoping for full participation from everyone. However, the above is a short-term project for the replacement of the existing fleets in the IAF. The LCH programme would cater to the long-term, larger needs of both the IAF and the Indian Army. A table to compare major attributes of the competing helicopters in the above mentioned RFP and that of the LCH has been given in the article.

If the flight-testing which would involve more than 500 flights, progresses without any major glitches, the Initial Operational Clearance (IOC) could be achieved by 2013 with an in-service induction by 2014. When operationalised, the LCH will give air-warriors the capability to engage targets at high altitudes, up to and even above 5,000 m, lack of which was sorely felt during the 1999 Kargil operations. During the unveiling ceremony on May 23, Ashok Nayak, Chairman, HAL, had revealed that the defence PSU already had a firm order from the IAF for 65 LCHs. The Indian Army has also evinced interest and in the long run could go in for 100 plus machines.

While it may be true that most of the helicopter’s sub-systems such as avionics packages and weapons may be imported, the indigenous design and systems integration could still peg the LCH as one of the most-competitive and cost-effective product in its class worldwide. Another much needed success story for the Indian aerospace industry.

Light Combat Helicopter

General/Performance Characteristics*
 

 General characteristics                                                              Performance

  Crew: 2   Never exceed speed: 330 km/h (178 knots, 207 mph)  
  Length: 15.8 m (51ft 8in)   Maximum speed: 275 km/h (148 knots, 171 mph)  
  Height: 4.7 m (15 ft 4 in)   Cruise speed: 260 km/h (140 knots, 161 mph)  
  Disc area: 138.9 m² (1472 ft²)   Range: 700km (297 nm, 342 mi)  
  Empty weight: 2550 kg (5621 lb)   Service ceiling: 6,500 m (21,300 ft)  
  Loaded weight: 4000 kg (8818 lb)   Rate of climb: 12 m/s (2362 ft/min)  
  Useful load: 2950 kg (6503 lb)   Disc loading: 39.59 kg/m² (8.23 lb/ft²)  
  Max takeoff weight: 5,700 kg (12125 lb)   Power/mass: 327 W/kg (0.198 hp/lb)  
  Power Plant: 2× Turbomeca/HAL TM333-2C2/Shakti turboshafts with FADEC,  871 kW (1200 hp) each        
 

 Armament

  Guns: M621 20 mm cannon on Nexter THL-20 turret  
  Rockets: Unguided rockets  
  Missiles: MBDA air-to-air missiles Air-to-surface missiles Anti-radiation missiles ATGM  
  Bombs: Iron bombs cluster bomb units grenade launcher  
 

 

Comparative Table

Attack Helicopters Major Attributes*
 
Manufacturer & Model Eurocopter EC665 Tiger AgustaWestland AW-129 Mangusta BELL AH-1Z Super Cobra Boeing AH-64 Apache Kamov Ka-50/52 Mil Mi-28N HAL Light Combat Helicopter (LCH)**
 Crew 2 (Pilot, WSO) 2 (Pilot, WSO) 2 (Pilot, WSO) 2 (Pilot, and co-pilot/gunner) 1(For Ka-52:tow) 2 (Pilot WSO) 2
 Rotor  Diameter(m) 13.00 11.90 14.6 14.63 2X14.50 17.20 13.3
 Waves (kg)  Empty / Max T/O 3,060/6000 2,530/4,600 5,580/8,390 5,165/10,433 7,800/10,800 7,890/12,100 2,250/5,700
 Power Plant 2 X Rolls Royce/ Turbomeca/ MTU MTR 390 Turboshafts 873 kW (1,170 shp ) each 2 X Rolls Royce Gem 2-1004D, Turboshafts 664 kW (890 shp) each 2 X General Electric T700-GE-401C Turboshafts, 1,340 kW (1,800 shp) each Latest 2 X General Electric T700- 701D 1,490 kW (2,086 shp) each 2X Kilmov TV3-117VK turboshafts 1,660 kW-(2,226 shp each) 2X Kilmov TV3-117VM turboshafts 1,640 KW (2,200 shp each) 2X Turbomeca/ HAL TM3332C2/ Shakti turboshafts with FADEC, 871 kW (1200 hp) each
 Max Speed (km/hr) 290 With Mast, 315 Without mast 278 411 365 390 377 275
 Service Ceiling (m) 4,000 4,725 6,100 6,400 5,500 5,750 6,500
 Range (km) 800 510 685 476 1,160 460 700
 Armament 1 X 30 mm cannon in chin turret plus podded guns SNEB rockets AGM-114 Hellfire Missiles Mistral AAMs 1X20 mm cannon, 4X rocket pods AGM-114 Hellfire or BGM-71N TOW anti-tank missiles AIM -92 Stinger or Mistral AAMs 1 X 3-barreled 20mm M197 Gatling In turret, 2.75 in rockets, AGM-114 Hellfire, AIM-9 Sidewinder AAMs 1 X30 X 113mm M230 Chain Gun, Hydra 70 FFAR rockets, AGM-114 Hellfire, AIM-9 Sidewinder and AIM-92 Stinger 1X30mm Shipunov 2A42 Cannon, gun pods, APU-6 9K121 Vikhr anti-tank missiles, high-calibre rockets, bombs, Vympel R-73 or Igla AAMs 1 X Chin Mounted 30mm Shipunov 2A42 cannon M621 20mm Cannon THL-20 turret, Unguided Rockets, MBDA AAMs ATGM Iron Bombs