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-1
Photo: Unknown author · Wikimedia Commons · Public domain
REC // INTEL FEED

MilMi-1

Utility / Transport Helicopters · Russia · 1951
ADD TO COMPARE

MilMi-1

Mil Mi-1
Mil Mi-1 Photo: Unknown author · Wikimedia Commons · Public domain
* Absolute score — assessed within category · no era adjustment
Payload / Capacity
30
Range
25
Versatility
40
Reliability
65
Speed
35
Survivability
20
Hot-and-High Performance
25
Maintainability
70
Technology
15
Cost-Effectiveness
75
Origin Russia
ManufacturerPZL-Świdnik
CategoryUtility / Transport Helicopters
EraEarly Cold War
In service1951–1965
Operators21 countries
Quantity2,594
Data Quality88%
39
Utility / Transport Helicopters MASS Rating
29/42
Early Cold War
183/208
All-Time
Utility / Transport Helicopters · 10 axes scored
Payload / Capacity
30
Range
25
Versatility
40
Reliability
65
Speed
35
Survivability
20
Hot-and-High Performance
25
Maintainability
70
Technology
15
Cost-Effectiveness
75
ⓘ Regardless of era, the same scoring system applies to all units in the utility / transport helicopters category.
01 / Overview
Mil Mi-1
Country
Prime contractor
Production
1951–1965
Quantity
2,594
Operators
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
UTILITY / TRANSPORT HELICOPTERS · EARLY COLD WAR
29
PERFORMANCE/PRICE
85
UNIT COST (2025 USD)
—
39
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 Flight1948
  • Service Entry Year1950
  • Crew2
  • Passengers3
  • Primary Rolelight utility and liaison helicopter
  • In ServiceYes
◈Powerplant8MOD.8
  • Engine TypeIvchenko AI-26V
  • Number of Engines1
  • Engine Power (each)428 kW
  • Transmission Rating428 kW
  • Rotor Configurationsingle main rotor with tail rotor
  • Main Rotor Diameter10 m
  • Main Rotor Blades2
  • Anti-Torque Typetail rotor
▣Performance10MOD.10
  • Top Speed170 km/h
  • Cruise Speed150 km/h
  • Never-Exceed Speed (VNE)210 km/h
  • Service Ceiling3,500 m
  • Hover Ceiling (IGE)2,500 m
  • Hover Ceiling (OGE)1,500 m
  • Range430 km
  • Ferry Range600 km
  • Rate of Climb5 m/s
  • Endurance120
◇Dimensions & Weights7MOD.7
  • Fuselage Length12.1 m
  • Height3.3 m
  • Rotor Disc Area78.5
  • Empty Weight1,760 kg
  • Max Takeoff Weight2,200 kg
  • Useful Load900 kg
  • Cabin Volume5
◆Armament & Mission7MOD.7
▲Production2MOD.2
  • Total Built2,594
  • Variants5
◎Service History3MOD.3
  • Production Start1950
  • Production End1965
  • Operational Statusretired in most former Soviet states, limited service elsewhere
03 / History
SERVICE LIFESPANStill in Service
  1. 1951Production started
  2. 1965Production ended
75
years in service
14
years in production
2,594
units produced
15
countries operating
ⓘ 6 countries retired it.
04 / Operators
📚 Sources
📖 ENCYCLOPEDIA Browse the Utility / Transport Helicopters entry →