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#1821

Mil Mi-2

🇷🇺 Soviet Union ·first flew 1961· utility helicopter

Mil Mi-2, photo 1 of 10
1/10 Radomil talk· CC BY-SA 3.0

what is it?

The Mil Mi-2 (NATO reporting name: Hoplite) is a small, three rotor blade Soviet-designed multi-purpose helicopter developed by the Mil Moscow Helicopter Plant, designed in the early 1960s and produced exclusively by WSK "PZL-Świdnik" in Poland. Nearly 5,500 were made by the time production stopped in 1999, and it remains in service globally.

How to recognise it: 2 turboshaft engines · 14.5 m main rotor

base stats

  • speed 200 km/htop speed
  • range 440 kmwithout refuelling
  • seats 8passengers
  • size 3,700 kgmax take-off weight
  • built 5,497made in total

Bars compare against all aircraft: 3,500 km/h, 20,000 km, 850 seats; size and number built on a log scale up to 640 t (An-225) and 45,000 built (Cessna 172).

fun facts

  • First flew 65 years ago, in 1961.
  • Top speed is 1.5× a car on the Dutch motorway (130 km/h).
  • Wingspan of 14.5 m: about 3 cars parked nose to tail.

turboshaft: A turbine that turns a shaft, usually a helicopter rotor.

spec sheet

first flight
1961-09-22
introduced
1965
status
still flying
number built
5,497
role
utility helicopter
origin
🇷🇺 Soviet Union
makers
PZL-Świdnik
engines
2× PZL GTD-350P / GTD-350
passengers
8
length
11.4 m
wingspan
14.5 m
rotor diameter
14.5 m
height
3.8 m
max take-off weight
3,700 kg
top speed
200 km/h
range
440 km
ceiling
4,000 m

Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.

Sources: Wikidata Q608997, Wikipedia: Mil Mi-2 (CC BY-SA 4.0).Updated 2026-10-24.

stan runge ef9524a source