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Ka-26family

Utility / Transport Helicopters · Russia · 1969
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Ka-26family

Ka-26 family
Ka-26 family Photo: Wikimedia Commons · Public domain
* Absolute score — assessed within category · no era adjustment
Payload / Capacity
40
Range
35
Versatility
55
Reliability
70
Speed
30
Survivability
25
Hot-and-High Performance
40
Maintainability
80
Technology
20
Cost-Effectiveness
85
Origin Russia
ManufacturerIndustria Aeronautică Română
CategoryUtility / Transport Helicopters
EraCold War
In service1969–1985
Operators8 countries
Quantity816
Data Quality87%
47
Utility / Transport Helicopters MASS Rating
51/61
Cold War
159/208
All-Time
Utility / Transport Helicopters · 10 axes scored
Payload / Capacity
40
Range
35
Versatility
55
Reliability
70
Speed
30
Survivability
25
Hot-and-High Performance
40
Maintainability
80
Technology
20
Cost-Effectiveness
85
ⓘ Regardless of era, the same scoring system applies to all units in the utility / transport helicopters category.
01 / Overview
Ka-26 family
Country
Production
1969–1985
Quantity
816
Operators
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
UTILITY / TRANSPORT HELICOPTERS · COLD WAR
51
PERFORMANCE/PRICE
90
UNIT COST (2025 USD)
—
47
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 Flight1965
  • Service Entry Year1969
  • Crew1
  • Passengers6
  • Primary RoleLight utility helicopter
  • In ServiceYes
◈Powerplant7MOD.7
  • Engine TypeVedeneyev M-14V-26
  • Number of Engines2
  • Engine Power (each)239 kW
  • Rotor ConfigurationCoaxial rotors
  • Main Rotor Diameter13 m
  • Main Rotor Blades3
  • Anti-Torque TypeCoaxial rotors
▣Performance9MOD.9
  • Top Speed170 km/h
  • Cruise Speed150 km/h
  • Service Ceiling3,000 m
  • Hover Ceiling (IGE)1,800 m
  • Hover Ceiling (OGE)1,500 m
  • Range400 km
  • Ferry Range1,200 km
  • Rate of Climb8 m/s
  • Endurance3
◇Dimensions & Weights7MOD.7
  • Fuselage Length7.75 m
  • Height4.05 m
  • Rotor Disc Area265.4
  • Empty Weight1,950 kg
  • Max Takeoff Weight3,076 kg
  • Useful Load1,300 kg
  • Cabin Volume3.5
◆Armament & Mission6MOD.6
▲Production2MOD.2
  • Total Built816
  • Variants5
◎Service History3MOD.3
  • Production Start1969
  • Production End1985
  • Operational StatusActive; out of production
03 / History
SERVICE LIFESPANStill in Service
  1. 1969Production started
  2. 1985Production ended
57
years in service
16
years in production
816
units produced
7
countries operating
ⓘ The producing country still actively operates it. 1 countries retired it.
04 / Operators
📚 Sources
📖 ENCYCLOPEDIA Browse the Utility / Transport Helicopters entry →