Mi-17 Hip-H vs SA 315B Lama
Overview
The Mi-17 Hip-H and the SA 315B Lama are both Military Helicopters, manufactured by Mil and Aérospatiale respectively.
Top speed is 250 km/h for the Mi-17 Hip-H vs 192 km/h for the SA 315B Lama. The Mi-17 Hip-H has an operational range of 800 km vs 515 km for the SA 315B Lama. The Mi-17 Hip-H operates at altitudes up to 6,000 m compared to 5,400 m for the SA 315B Lama. At 13,000 kg MTOW, the Mi-17 Hip-H is 5.7x the SA 315B Lama's 2,300 kg.
The Mi-17 Hip-H has been produced in 12,000 units vs 400 for the SA 315B Lama. The SA 315B Lama first flew 6 years before the Mi-17 Hip-H (1969 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 single-engined utility helicopter, developed in the late 1960s and introduced in the early 1970s, designed specifically for exceptional high-altitude operations. | |
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| Origin country | 🇫🇷 France |
| Category | Military Helicopters |
| Manufacturer | Aérospatiale |
| First flight | 17 March 1969 |
| Year introduced | 1971 |
| Number produced | 400 units |
| Average unit price | -- |
| Wing area | -- m² |
| 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 ◉ |
| Wing area | 95.4 m² |
| Wingspan | 11.0 m ◉ |
| Height | 3.1 m ◉ |
| Length | 10.2 m ◉ |
| Maximum speed | 192 km/h ◉ |
| Operational range | 515 km ◉ |
| Service ceiling | 5,400 m ◉ |
| Max. takeoff weight | 2,300 kg ◉ |
| Empty weight | 1,021 kg ◉ |
| Total thrust | 1 x 649 kW ◉ |
Performance Radar Chart
Detailed Comparison
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Frequently Asked Questions
Which is faster, the Mi-17 Hip-H or SA 315B Lama?
The Mi-17 Hip-H is faster with a maximum speed of 250 km/h compared to the SA 315B Lama's 192 km/h, a difference of 58 km/h.
Which has longer range, the Mi-17 Hip-H or SA 315B Lama?
The Mi-17 Hip-H has a longer range at 800 km compared to the SA 315B Lama's 515 km.
Which can fly higher, the Mi-17 Hip-H or SA 315B Lama?
The Mi-17 Hip-H has a higher service ceiling at 6,000 meters (19,685 ft) compared to the SA 315B Lama's 5,400 meters (17,716 ft).
Which is heavier, the Mi-17 Hip-H or SA 315B Lama?
The Mi-17 Hip-H has a higher maximum takeoff weight at 13,000 kg compared to the SA 315B Lama's 2,300 kg.
Which is larger, the Mi-17 Hip-H or SA 315B Lama?
The Mi-17 Hip-H is longer at 18.5 meters compared to the SA 315B Lama's 10.2 meters.
Which entered service first, the Mi-17 Hip-H or SA 315B Lama?
The SA 315B Lama entered service first in 1971, 6 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 SA 315B Lama?
The Mi-17 Hip-H has been produced in greater numbers with 12,000 units compared to 400 units of the SA 315B Lama.