The Puma medium lift helicopter was in production until 1987 featuring many roles including military and civilian. Used in the army as a troop carrier it could seat twelve occupants. As a civilian based helicopter the Puma could seat twenty passengers. A total of 696 Puma's had been sold by the end of manufacture although they are still produced in Romania. The Puma was built by the EUROCOPTER Group, owned 70% by AEROSPATIALE France and 30% by Daimler Aerospace (DASA) of Germany.
The Cougar name was adopted for all military variants, and in 1990, all Super Puma designations were changed from AS 332 to AS 532 to distinguish between civil and military variants. The Cougar was designed to provide high performance, ease of deployment, low operating cost, comfort, plus high mission readiness. For military use and adapting to modern battlefield conditions, it features survivability, suitability for tactical flight thanks to exceptional manoeuvrability, low observability, low vulnerability to projectiles, crashworthiness. A multirole helicopter, the Cougar can be armed with machine-guns and pod-mounted cannons, with rockets, or with antisubmarine or antisurface weapon systems to suit different mission requirements. Additional missions include: VIP transport, electronic warfare, and anti-submarine warfare.
The large, four-blade main rotor is mounted above center of fuselage on a hump. Two turboshaft engines are mounted on top of the fuselage midsection, giving the helicopter a humpbacked appearance. The fuselage is long, rectangular, upswept, with a tapered rear section, a rounded, stepped-up, glassed-in cockpit and retractable landing gear. Swept-back and tapered tail fin mounts a rotor on the right and a tapered, single flat on left top of the fin.
The Turbomeca Makila 1A1 turboshafts engines, of modular design and low specific fuel consumption, endows the Cougar with impressive power (2 x 1877 shp). Coupled with exceptionally short response times, contributing to the machine's tactical flight capability. The rotors blades are made of composite materials throughout. By comparison with blades incorporating metallic components, this makes for unsurpassed serviceability, low vulnerability, an unlimited useful life and imperviousness to marine corrosion. Other innovations include a simplified main rotor hub, a main gearbox of modular design and a high-energy-absorption landing-gear contributing to the machine's crashworthiness. The Cougar can also be equipped with jet diluters for protection against heat-seeking missiles, with infrared and electromagnetic countermeasures, crashworthy seats for pilot and military personnel, armorplate for crew seats and vital parts of the machine, a 4.5 metric-ton capacity sling and a winch capable of hoisting 245 kg.
Specifications | |
Country of Origin | France/Germany |
Builder | EUROCOPTER [AEROSPATIALE & DASA] |
Role | Armed transport |
Similar Aircraft | Super Frelon, HH-3E Jolly Green Giant, SH-3 Sea King, CH-53 Sea Stallion, Mi-8 Hip, UH-60 Black Hawk |
Date of Introduction | 1981 |
Blades |
Main rotor: 4 Tail rotor: 5, 4 (U2/A2) |
Rotor Diameter |
Main Rotor : 14 m (Puma) 15.6-16.2 m (U2/A2) Tail Rotor : 3.1-3.2 m (U2/A2) |
Length |
18.7-19.5 m (U2/A2) (rotors turning) 15.5 m (UC/AC), 16.3 m (UL/AL), 16.8 m (U2/A2) (fuselage) |
Height | 4.6 m |
Width | 3.6-3.8 m (U2/A2) |
Cargo Compartment |
Floor Length: 6.5 m (AC/UC), 6.8 m (UL/AL), 7.9 m (U2/A2) Width: 1.8 m Height: 1.5 |
Weight |
Maximum Gross: 9,000 kg (Mk I), 9,750 kg (Mk II) Normal Takeoff: 8,600 kg (Mk I), 9,300 kg (Mk II) Empty: 4,330 kg (UC/AC), 4,460 kg (UL/AL), 4,760 kg (U2/A2) |
Standard Payload |
Internal load: 3,000 kg External on sling only: 4,500 kg Transports 20-29 troops or 6-12 litters (variant dependant), or cargo. |
Engine | 2x 1,877-shp Turbomeca Makila 1A1 turboshaft |
Maximum speed | 275 km/h (Mk I), 325 km/h (Mk II) |
Cruising speed | 249-270 km/h |
Range | 769 km-416 n.m. 800 km-432 n.m AS 532 UL/AL Normal Load: 620 km (UC/AC), 840 km (UL/AL), 800 km (U2/A2) With Aux Fuel: 1,017 km (UC/AC), 1, 245 km (UL/AL), 1,176 km (U2/A2) |
Fuel |
Internal: 1,497 liters (UC/AC), 2,000 liters (UL/AL), 2,020 liters (U2/A2) Internal Aux Tank: 475 liters ea. (4x Mk I, 5xMk II) |
Service Ceiling | 4,100 m |
Hover |
out of ground effect: 1,650 m (Mk I), 1,900 m (Mk II) in ground effect: 2,800 m (Mk I), 2,540 m (Mk II) |
Vertical Climb Rate | 7 m/s |
Armament |
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Survivability/Countermeasures | Main and tail rotor blades electrically deiced. A radar warning receiver is standard, while a laser warning receiver, missile launch detector, missile approach detector, infrared jammer, decoy launcher, and flare/chaff dispensers are optionally available. |
Special equipment | Armour plates for the cargo, PLS (Personal Locator System), GPS (Global Positioning System), chaff/flare dispensers, RWR (radar warning receiver), MWS (Missile approach warning system) |
AVIONICS | The aircraft is NVG compatible, and through its instruments, avionics, full autopilot, and nav computer, is capable of operation in day, night, and instrument meteorological conditions. |
Crew | 2 (pilots) |
Cost | |
User Countries | At least 38 countries : Algeria, Argentina, Belgium, Brazil, Chad, Chile, China, Djibouti, Ecuador, France, Gabon, Germany, Iceland, Indonesia, Iraq, Ivory Coast, Jordan, Kenya, Kuwait, Lebanon, Libya, Malawi, Mexico, Morocco, Nepal, Nigeria, Oman, Pakistan, Panama, Philippines, Portugal, Senegal, Singapore, South Africa, Spain, Sudan, Switzerland, Togo, United Arab Emirates, UK, Zaire |