Mi-8 Hip vs SA 315B Lama
Overview
The Mi-8 Hip and the SA 315B Lama are both Military Helicopters, manufactured by Mil and Aérospatiale respectively.
Top speed is 250 km/h for the Mi-8 Hip vs 192 km/h for the SA 315B Lama. The Mi-8 Hip has an operational range of 495 km vs 515 km for the SA 315B Lama. The SA 315B Lama operates at altitudes up to 5,400 m compared to 4,500 m for the Mi-8 Hip. At 12,000 kg MTOW, the Mi-8 Hip is 5.2x the SA 315B Lama's 2,300 kg.
The Mi-8 Hip has been produced in 17,000 units vs 400 for the SA 315B Lama. The Mi-8 Hip first flew 8 years before the SA 315B Lama (1961 vs 1969).
| Soviet multipurpose helicopter, prevalent during the Cold War, extensively utilized for transport, combat and humanitarian operations globally. | |
|
|
| Origin country | 🇨🇳 Ex-USSR |
| Category | Military Helicopters |
| Manufacturer | Mil |
| First flight | 24 June 1961 |
| Year introduced | 1967 |
| Number produced | 17000 units |
| Average unit price | $4 million |
| French single-engined utility helicopter, developed in the late 1960s and introduced in the early 1970s, designed specifically for exceptional high-altitude operations. | |
|
|
| 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 | 5.7 m ◉ |
| Length | 25.2 m ◉ |
| Maximum speed | 250 km/h ◉ |
| Operational range | 495 km ◉ |
| Service ceiling | 4,500 m ◉ |
| Max. takeoff weight | 12,000 kg ◉ |
| Empty weight | 7,160 kg ◉ |
| Total thrust | 2 x 560 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
Loading analysis...
Generating comparison analysis...
Unable to generate comparison at this time.
Frequently Asked Questions
Which is faster, the Mi-8 Hip or SA 315B Lama?
The Mi-8 Hip 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-8 Hip or SA 315B Lama?
The SA 315B Lama has a longer range at 515 km compared to the Mi-8 Hip's 495 km.
Which can fly higher, the Mi-8 Hip or SA 315B Lama?
The SA 315B Lama has a higher service ceiling at 5,400 meters (17,716 ft) compared to the Mi-8 Hip's 4,500 meters (14,763 ft).
Which is heavier, the Mi-8 Hip or SA 315B Lama?
The Mi-8 Hip has a higher maximum takeoff weight at 12,000 kg compared to the SA 315B Lama's 2,300 kg.
Which is larger, the Mi-8 Hip or SA 315B Lama?
The Mi-8 Hip is longer at 25.2 meters compared to the SA 315B Lama's 10.2 meters.
Which entered service first, the Mi-8 Hip or SA 315B Lama?
The Mi-8 Hip entered service first in 1967, 4 years before the SA 315B Lama which entered service in 1971.
Which has been built in greater numbers, the Mi-8 Hip or SA 315B Lama?
The Mi-8 Hip has been produced in greater numbers with 17,000 units compared to 400 units of the SA 315B Lama.