LATEST Ancient Prototypes of Proxy Warfare: The Economic and Logistical Burden of Roman and Persian Proxy Networks among Arab Tribes and Caucasian Powers
SEARCH
DB ONLINE
EN ▾
Mil Mi-4
Photo: Jan Hrdonka · Wikimedia Commons · CC BY-SA 4.0
REC // INTEL FEED

MilMi-4

Utility / Transport Helicopters · Russia · 1951
ADD TO COMPARE

MilMi-4

Mil Mi-4
Mil Mi-4 Photo: Jan Hrdonka · Wikimedia Commons · CC BY-SA 4.0
* Absolute score — assessed within category · no era adjustment
Payload / Capacity
60
Range
55
Versatility
65
Reliability
70
Speed
50
Survivability
40
Hot-and-High Performance
55
Maintainability
75
Technology
45
Cost-Effectiveness
80
Origin Russia
CategoryUtility / Transport Helicopters
EraEarly Cold War
In service1951–1979
Operators29 countries
Quantity4,000
Data Quality88%
60
Utility / Transport Helicopters MASS Rating
15/42
Early Cold War
130/208
All-Time
Utility / Transport Helicopters · 10 axes scored
Payload / Capacity
60
Range
55
Versatility
65
Reliability
70
Speed
50
Survivability
40
Hot-and-High Performance
55
Maintainability
75
Technology
45
Cost-Effectiveness
80
ⓘ Regardless of era, the same scoring system applies to all units in the utility / transport helicopters category.
01 / Overview
Mil Mi-4
Country
Production
1951–1979
Quantity
4,000
Operators
Conflicts
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
UTILITY / TRANSPORT HELICOPTERS · EARLY COLD WAR
15
PERFORMANCE/PRICE
85
UNIT COST (2025 USD)
—
60
utility / transport helicopters category
ⓘ Performance/Price and MASS score are computed across all units in the utility / transport helicopters category, regardless of era.
02 / Specs & Design
◎General6MOD.6
  • First Flight1951
  • Service Entry Year1952
  • Crew2
  • Passengers11
  • Primary RoleTransport helicopter
  • In ServiceYes
◈Powerplant8MOD.8
  • Engine TypeShvetsov ASh-82V
  • Number of Engines1
  • Engine Power (each)1,430 kW
  • Transmission Rating1,430 kW
  • Rotor ConfigurationSingle main rotor with tail rotor
  • Main Rotor Diameter21 m
  • Main Rotor Blades4
  • Anti-Torque TypeTail rotor
▣Performance10MOD.10
  • Top Speed180 km/h
  • Cruise Speed180 km/h
  • Never-Exceed Speed (VNE)210 km/h
  • Service Ceiling5,450 m
  • Hover Ceiling (IGE)1,760 m
  • Hover Ceiling (OGE)1,250 m
  • Range430 km
  • Ferry Range650 km
  • Rate of Climb5.6 m/s
  • Endurance135
◇Dimensions & Weights7MOD.7
  • Fuselage Length16.79 m
  • Height4.4 m
  • Rotor Disc Area346.36
  • Empty Weight3,020 kg
  • Max Takeoff Weight7,350 kg
  • Useful Load4,330 kg
  • Cabin Volume12.2
◆Armament & Mission8MOD.8
▲Production2MOD.2
  • Total Built3,259
  • Variants10
◎Service History4MOD.4
  • Retirement Year1991
  • Production Start1952
  • Production End1969
  • Operational StatusLimited Service; North Korean Air Force
03 / History
SERVICE LIFESPANStill in Service
  1. 1945First deployment: Cold War
  2. 1951Production started
  3. 1952Entered service
  4. 1957Sale: Albania (7 units)
  5. 1961Sale: Cuba (85 units)
  6. 1974Sale: Cuba
  7. 1979Production ended
75
years in service
28
years in production
4,000
units produced
16
countries operating
ⓘ The producing country no longer actively operates it. 13 countries retired it.
04 / Conflicts
MIL MI-4 · CONFLICTS SERVED IN0% win
Total Conflicts
1
Victories
0
Ongoing
0
Losses
0
ⓘ Shown only from conflicts recorded in our database.
05 / Operators
Operator Inventory2country · 92units
92active
Mil Mi-4SALES3records
YearBuyerQuantityAmountPresent Value (2025)
1974Cuba———
1961Cuba85——
1957Albania7——
ⓘ "Present Value" is an estimated amount adjusted for inflation.
📖 TERMS ON THIS PAGE2terms
A mechanical device used to lift personnel or cargo via a cable, typically mounted on helicopters for rescue or recovery operations.
Aerodynamic containers mounted on aircraft, typically helicopters or fighter jets, that hold and launch unguided rockets in rapid succession.
These terms are listed automatically because they appear on this page.full encyclopedia →
📚 Sources
📖 ENCYCLOPEDIA Browse the Utility / Transport Helicopters entry →