Mi-17 Hip-H vs SA321 Super Frelon
Overview
The Mi-17 Hip-H and the SA321 Super Frelon are both Military Helicopters, manufactured by Mil and Aérospatiale respectively.
Top speed is 250 km/h for the Mi-17 Hip-H vs 275 km/h for the SA321 Super Frelon. The Mi-17 Hip-H has an operational range of 800 km vs 1,020 km for the SA321 Super Frelon. The Mi-17 Hip-H operates at altitudes up to 6,000 m compared to 3,100 m for the SA321 Super Frelon.
The Mi-17 Hip-H has been produced in 12,000 units vs 110 for the SA321 Super Frelon. Unit cost is $15M for the Mi-17 Hip-H vs $3.5M for the SA321 Super Frelon. The SA321 Super Frelon first flew 13 years before the Mi-17 Hip-H (1962 vs 1975).
| Soviet transport helicopter, prominently deployed during Afghan War, globally used for cargo, troop transport, and rescue missions. | |
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| Origin country | 🇨🇳 Ex-USSR |
| Category | Military Helicopters |
| Manufacturer | Mil |
| First flight | 1 January 1975 |
| Year introduced | 1977 |
| Number produced | 12000 units |
| Average unit price | $15 million |
| French heavy transport helicopter, operational during the Cold War, prominently used by China, France, and Israel. | |
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| Origin country | 🇫🇷 France |
| Category | Military Helicopters |
| Manufacturer | Aérospatiale |
| First flight | 7 December 1962 |
| Year introduced | 1966 |
| Number produced | 110 units |
| Average unit price | $3.5 million |
| Wingspan | 21.3 m ◉ |
| Height | 4.8 m ◉ |
| Length | 18.5 m ◉ |
| Maximum speed | 250 km/h ◉ |
| Operational range | 800 km ◉ |
| Service ceiling | 6,000 m ◉ |
| Max. takeoff weight | 13,000 kg ◉ |
| Empty weight | 7,489 kg ◉ |
| Total thrust | 2 x 746 kW ◉ |
| Wingspan | 18.9 m ◉ |
| Height | 6.7 m ◉ |
| Length | 23.0 m ◉ |
| Maximum speed | 275 km/h ◉ |
| Operational range | 1,020 km ◉ |
| Service ceiling | 3,100 m ◉ |
| Max. takeoff weight | 13,000 kg ◉ |
| Empty weight | 6,865 kg ◉ |
| Total thrust | 3 x 385 kW ◉ |
Performance Radar Chart
Detailed Comparison
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Frequently Asked Questions
Which is faster, the Mi-17 Hip-H or SA321 Super Frelon?
The SA321 Super Frelon is faster with a maximum speed of 275 km/h compared to the Mi-17 Hip-H's 250 km/h, a difference of 25 km/h.
Which has longer range, the Mi-17 Hip-H or SA321 Super Frelon?
The SA321 Super Frelon has a longer range at 1,020 km compared to the Mi-17 Hip-H's 800 km.
Which can fly higher, the Mi-17 Hip-H or SA321 Super Frelon?
The Mi-17 Hip-H has a higher service ceiling at 6,000 meters (19,685 ft) compared to the SA321 Super Frelon's 3,100 meters (10,170 ft).
Which is heavier, the Mi-17 Hip-H or SA321 Super Frelon?
The SA321 Super Frelon has a higher maximum takeoff weight at 13,000 kg compared to the Mi-17 Hip-H's 13,000 kg.
Which is larger, the Mi-17 Hip-H or SA321 Super Frelon?
The SA321 Super Frelon is longer at 23.0 meters compared to the Mi-17 Hip-H's 18.5 meters.
Which is more expensive, the Mi-17 Hip-H or SA321 Super Frelon?
The Mi-17 Hip-H is more expensive at approximately $15 million per unit compared to the SA321 Super Frelon at $3.5 million.
Which entered service first, the Mi-17 Hip-H or SA321 Super Frelon?
The SA321 Super Frelon entered service first in 1966, 11 years before the Mi-17 Hip-H which entered service in 1977.
Which has been built in greater numbers, the Mi-17 Hip-H or SA321 Super Frelon?
The Mi-17 Hip-H has been produced in greater numbers with 12,000 units compared to 110 units of the SA321 Super Frelon.