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HAL Dhruv (Polaris)

India (2002)
National Flag Graphic
Origin: India
Year: 2002
Type: Multirole Medium-Lift Transport Helicopter
Manufacturer(s): Hindustan Aeronautics Limited (HAL) - India
Production: 200
Status: Active, In-Service


The HAL Dhruv is currently in service with Indian armed forces and has found customers in several countries around the world.


Detailing the development and operational history of the HAL Dhruv (Polaris) Multirole Medium-Lift Transport Helicopter.  Entry last updated on 5/15/2018. Authored by Staff Writer. Content ©www.MilitaryFactory.com

While still largely reliant on foreign suppliers, the Indian military industry has made strides in developing internal solutions to ongoing requirements. Hindustan Aeronautics Limited (HAL) has developed the "Dhruv" (meaning "Polaris") as a multirole, medium-lift helicopter to serve the Army, Air Force and Navy. Some 200 of the type have since been produced. Its armed combat version is the HAL "Rudra".

The Dhruv was unveiled in late 1984 and this stemmed from a 1979 requirement for a multirole military helicopter in the five-ton range. The process involved foreign assistance from the MBB concern of Germany - then West Germany. First flight was recorded on August 20th, 1992. However, the development phase was fraught with delays by way of technological challenges, sanctions, changing Army requirements (and its general commitment) and internal economic issues - its first flight was actually scheduled for 1989. This led to the platform finally attaining service introduction in March of 2002.

Another setback proved to be the engine of choice - the American LHTEC T800 turboshaft - which fell under embargo. This forced engineers to select a French-originated model in the Turbomeca TM333-2B2 turboshaft of 1,000 horsepower (India has held a close relationship with both France and Russia in recent decades). The selection of the French engine then involved assistance from French engineers which benefitted the program considerably.

At its core, the Dhruv is a largely conventional multirole platform. It sports a well-glazed cockpit seating two in a side-by-side arrangement. Aft of the cockpit is the passenger seating area straddled along either side by sliding access doors. The engines sit atop the cabin roof in the usual way and drive a four-bladed composite main rotor (low mounted) as well as a four-bladed tail rotor (by way of an extension shaft in the tail stem) fitted to the starboard side. The undercarriage is fixed as a twin skid assembly for simplicity in operation and repair though some versions have been seen with a retractable wheeled undercarriage as well. The raised tail stem allows a clamshell type access door to be fitted at the fuselage rear. The tail unit also contains a vertical fin (which mounts the drive gear for the tail rotor) and low-mounted horizontal planes (containing smaller vertical tail fins).

The Dhruv military form first appeared through the Mk.1 designation and this was a crude form of the intended design, featuring a mechanical-gauged cockpit. Production of these began in 2001 and some 56 were delivered. The Mk.2 introduced a locally-designed and developed (by HAL) all-glass cockpit for a more modern look. These were largely faithful to the Mk.1 version save for its advanced internals and production began in 2007. The Mk.3 was given uprated engines ("Shakti" engines of 1,200 horsepower), an improved countermeasures fit (chaff and flare dispensers), improved Electronic Warfare (EW) equipment, increased survivability and vibration control solutions. Introduction of this form came in 2012. The Mk.4 "Rudra" is the aforementioned armed combat model featuring an integrated weapons system.

The Dhruv also exists along civilian market lines in the C, CFW and CS models. These can seat as many as twelve passengers and have been in service since late 2003. The helicopter is in military service with (or scheduled to enter service with) the governments of Ecuador, India, Israel, Maldives, Mauritius, Nepal and Suriname. In civilian airspace, the Dhruv has been seen in (or ordered by) India, Turkey and Peru. First export customers were Nepal and Israel.

Any available statistics for the HAL Dhruv (Polaris) Multirole Medium-Lift Transport Helicopter are showcased in the areas immediately below. Categories include basic specifications covering country-of-origin, operational status, manufacture(s) and total quantitative production. Other qualities showcased are related to structural values (namely dimensions), installed power and standard day performance figures, installed or proposed armament and mission equipment (if any), global users (from A-to-Z) and series model variants (if any).






Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.

Image of collection of graph types

Relative Maximum Speed Rating
Hi: 200mph
Lo: 100mph
    This entry's maximum listed speed (174mph).

    Graph average of 150 miles-per-hour.
City-to-City Ranges
NYC
 
  LON
LON
 
  PAR
PAR
 
  BER
BER
 
  MOS
MOS
 
  TOK
TOK
 
  SYD
SYD
 
  LAX
LAX
 
  NYC
Graph showcases the HAL Dhruv's operational range (on internal fuel) when compared to distances between major cities.
Aviation Era
Pie graph section
Pie graph section
Pie graph section
Pie graph section
Pie graph section
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Unit Production Comparison
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units
200
200


  * Commercial Market High belongs to Cessna 172.

  ** Military Market High belongs to Ilyushin Il-2.


Altitude Visualization
Small airplane graphic
  Compare this entry against other aircraft using our Comparison Tool  
Global Operators:
Bolivia; Burma; Ecuador; India; Israel; Maldives; Mauritus; Nepal; Peru; Suriname; Turkey
Historical Commitments / Honors:

Military lapel ribbon for Operation Allied Force
Military lapel ribbon for the Arab-Israeli War
Military lapel ribbon for the Battle of Britain
Military lapel ribbon for the Battle of Midway
Military lapel ribbon for the Berlin Airlift
Military lapel ribbon for the Chaco War
Military lapel ribbon for the Cold War
Military lapel ribbon for the Cuban Missile Crisis
Military lapel ribbon for the Falklands War
Military lapel ribbon for the French-Indochina War
Military lapel ribbon for the Golden Age of Flight
Military lapel ribbon for the 1991 Gulf War
Military lapel ribbon for the Indo-Pak Wars
Military lapel ribbon for the Iran-Iraq War
Military lapel ribbon for the Korean War
Military lapel ribbon for the 1982 Lebanon War
Military lapel ribbon for the Malayan Emergency
Military lapel ribbon for the attack on Pearl Harbor
Military lapel ribbon for the Six Day War
Military lapel ribbon for the Soviet-Afghan War
Military lapel ribbon for the Spanish Civil War
Military lapel ribbon for the Suez Crisis
Military lapel ribbon for the Vietnam War
Military lapel ribbon for Warsaw Pact of the Cold War-era
Military lapel ribbon for the WASP (WW2)
Military lapel ribbon for the World War 1
Military lapel ribbon for the World War 2
Military lapel ribbon for the Yom Kippur
* Ribbons not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective campaigns/operations.
Measurements and Weights icon
Structural - Crew, Dimensions, and Weights:
Unless otherwise noted the presented statistics below pertain to the HAL Dhruv model. Common measurements, and their respective conversions, are shown when possible.

Operational
CREW


Personnel
2


Dimension
LENGTH


Feet
52.07 ft


Meters
15.87 m


Dimension
WIDTH


Feet
43.31 ft


Meters
13.2 m


Dimension
HEIGHT


Feet
13.29 ft


Meters
4.05 m


Weight
EMPTY


Pounds
5,516 lb


Kilograms
2,502 kg


Weight
LOADED


Pounds
12,125 lb


Kilograms
5,500 kg

Engine icon
Installed Power - Standard Day Performance:
2 x Shakti turboshaft engine developing 1,200 horsepower OR 2 x Turbomeca TM 333-2B2 turboshaft engines developing 1,000 horsepower each while driving a four-blade main rotor and a four-blade tail rotor.

Performance
SPEED


Miles-per-Hour
174 mph


Kilometers-per-Hour
280 kph


Knots
151 kts


Performance
RANGE


Miles
514 mi


Kilometers
827 km


Nautical Miles
447 nm


Performance
CEILING


Feet
27,500 ft


Meters
8,382 m


Miles
5.21 mi


Performance
CLIMB RATE


Feet-per-Minute
1,771 ft/min


Meters-per-Minute
540 m/min

Supported Weapon Systems:

Graphical image of an aircraft rocket pod
Graphical image of an aircraft aerial torpedo
Armament - Hardpoints (4):

OPTIONAL (Armed Variant):
8 x Anti-tank missiles
4 x 68mm rocket pods
2 x Torpedoes
2 x Depth charges
4 x Anti-ship missiles
Variants: Series Model Variants
• Dhruv - Base Series Production Designation
• Rudra - Armed Combat Variant of the Dhruv