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H215M / AS532 Cougar vs Mi-8 Hip

H215M / AS532 Cougar vs Mi-8 Hip at a glance — top speed 250 vs 250 km/h, range 573 vs 495 km, max takeoff weight 9,000 vs 12,000 kg, built 408 vs 17,000 units.

Airbus Helicopters H215M / AS532 Cougar military helicopters side profile drawing
🇩🇪🇫🇷 H215M / AS532 Cougar
Mil Mi-8 Hip military helicopters side profile drawing
🇷🇺 Mi-8 Hip
Specifications
H215M / AS532 Cougar Mi-8 Hip
Origin country 🇩🇪 Germany🇫🇷 France 🇷🇺 Ex-USSR
Category Military Helicopters Military Helicopters
Manufacturer Airbus Helicopters Mil
First flight 1 September 1978 24 June 1961
Year introduced 1978 1967
Number produced 408 units 17000 units
Average unit price $18 million $4 million
Wingspan 15.6 m 21.3 m
Height 4.8 m 5.7 m
Length 18.7 m 25.2 m
Maximum speed 250 km/h 250 km/h
Operational range 573 km 495 km
Service ceiling 4,100 m 4,500 m
Max. takeoff weight 9,000 kg 12,000 kg
Empty weight 4,330 kg 7,160 kg
Total thrust 2 x 1,185 kW 2 x 1,119 kW
Performance Radar Chart

Detailed Comparison

The Airbus H215M (formerly AS532 Cougar) and the Mil Mi-8 Hip represent the divergent rotary-wing doctrines of Western Europe and the Soviet Bloc. While the Cougar offers a lighter, avionics-driven multi-role platform, the Mi-8 serves as a heavy-lifting workhorse defined by sheer ruggedness and ubiquity. The Cougar is a specialized evolution of the medium-weight Puma, whereas the Mi-8 is a foundational mass-production airframe that bridges the gap between medium utility and heavy transport.

Development and Design

The H215M design utilizes composite rotor blades, crashworthy landing gear, and twin Turbomeca Makila engines, reflecting a philosophy centered on survivability through advanced materials and systems. It is highly adaptable, accommodating specialized naval avionics, including ASIST for high sea state operations. Conversely, the Mi-8 features a robust, largely aluminum airframe designed for austere field maintenance and ease of repair. Its distinctive top-mounted turbines and five-blade main rotor prioritize raw lift and stability over aerodynamic refinement. While the Cougar is a dedicated militarized derivative of a civil platform, the Mi-8 was conceived from the onset as a dual-purpose battlefield asset, capable of transforming from a troop carrier into a heavily armed gunship with window-mounted machine guns and external hardpoints.

Specifications and Performances

The Mi-8 holds a significant advantage in lift capacity, with a Maximum Takeoff Weight (MTOW) of 12,000 kg compared to the Cougar's 9,000 kg. This allows the Hip to transport heavier logistics or larger troop contingents. However, the H215M demonstrates superior aerodynamic efficiency; despite sharing a maximum speed of 250 km/h, the Cougar offers a longer operational range of 573 km versus the Mi-8's 495 km. The Cougar's lighter empty weight (4,330 kg) against the massive Mi-8 (7,160 kg) allows for greater agility and a better power-to-weight ratio for technical maneuvering, whereas the Hip's mass provides a stable firing platform for heavy weaponry.

Deployment and Usage

Deployment of the AS532/H215M leans toward specialized roles, particularly in naval environments where it employs AM 39 Exocet missiles and variable-depth sonar for Anti-Submarine Warfare (ASW). It serves as a sophisticated asset for modern armies requiring avionics standardization, as seen in France's fleet upgrades. The Mi-8, with over 17,000 units built, functions as the logistical backbone for over 50 nations. It operates extensively in "hot-and-high" theaters like Afghanistan, serving simultaneously as a troop transport and fire support platform armed with S-8 rockets and AT-2 Swatter missiles. While the Cougar is often protected in hangars, the Mi-8 is designed to live on the tarmac in extreme climates.

Conclusion

The choice between these aircraft dictates the operational doctrine. The H215M provides a high-tech solution for NATO-standard forces requiring specialized mission equipment and lower acoustic signatures, albeit at a significantly higher unit cost of $18 million. The Mi-8, priced at approximately $4 million, offers unmatched logistical volume and durability for budget-constrained forces needing a resilient, do-it-all platform. The Cougar excels in precision and multi-role versatility, while the Hip remains the superior option for raw utility and heavy lift in contested environments.

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Frequently Asked Questions

Which is faster, the H215M / AS532 Cougar or Mi-8 Hip?
The Mi-8 Hip is faster with a maximum speed of 250 km/h compared to the H215M / AS532 Cougar's 250 km/h, a difference of 0 km/h.
Which has longer range, the H215M / AS532 Cougar or Mi-8 Hip?
The H215M / AS532 Cougar has a longer range at 573 km compared to the Mi-8 Hip's 495 km.
Which can fly higher, the H215M / AS532 Cougar or Mi-8 Hip?
The Mi-8 Hip has a higher service ceiling at 4,500 meters (14,763 ft) compared to the H215M / AS532 Cougar's 4,100 meters (13,451 ft).
Which is heavier, the H215M / AS532 Cougar or Mi-8 Hip?
The Mi-8 Hip has a higher maximum takeoff weight at 12,000 kg compared to the H215M / AS532 Cougar's 9,000 kg.
Which is larger, the H215M / AS532 Cougar or Mi-8 Hip?
The Mi-8 Hip is longer at 25.2 meters compared to the H215M / AS532 Cougar's 18.7 meters.
Which is more expensive, the H215M / AS532 Cougar or Mi-8 Hip?
The H215M / AS532 Cougar is more expensive at approximately $18 million per unit compared to the Mi-8 Hip at $4.0 million.
Which entered service first, the H215M / AS532 Cougar or Mi-8 Hip?
The Mi-8 Hip entered service first in 1967, 11 years before the H215M / AS532 Cougar which entered service in 1978.
Which has been built in greater numbers, the H215M / AS532 Cougar or Mi-8 Hip?
The Mi-8 Hip has been produced in greater numbers with 17,000 units compared to 408 units of the H215M / AS532 Cougar.