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Douglas C-124 Globemaster II
Photo: USAF · Wikimedia Commons · Public domain
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DouglasC-124GlobemasterII

Tactical Transports · United States · 1950
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DouglasC-124GlobemasterII

Douglas C-124 Globemaster II
Douglas C-124 Globemaster II Photo: USAF · Wikimedia Commons · Public domain
* Absolute score — assessed within category · no era adjustment
Payload
85
Short / Rough-Field Capability
60
Range
70
Cargo Versatility
80
Reliability
75
Self-Protection
30
Low-Altitude Capability
65
Versatility
70
Technology
60
Cost-Effectiveness
70
Origin United States
ManufacturerDouglas
CategoryTactical Transports
EraEarly Cold War
In service1950–1955
Operators1 countries
Quantity448
Data Quality87%
MASS(Military Archive Scoring System)
68
Tactical Transports MASS Rating
16/60
Early Cold War
62/215
All-Time
Tactical Transports · 10 axes scored
Payload
85
Short / Rough-Field Capability
60
Range
70
Cargo Versatility
80
Reliability
75
Self-Protection
30
Low-Altitude Capability
65
Versatility
70
Technology
60
Cost-Effectiveness
70
ⓘ Regardless of era, the same scoring system applies to all units in the tactical transports category.
01 / Overview
Douglas C-124 Globemaster II
Prime contractor
Production
1950–1955
Quantity
448
Operators
Conflicts
💰 PERFORMANCE / PRICE ASSESSMENT Methodology ↗
TACTICAL TRANSPORTS · EARLY COLD WAR
16
PERFORMANCE/PRICE
75
UNIT COST (2025 USD)
—
68
tactical transports category
ⓘ Performance/Price and MASS score are computed across all units in the tactical transports category, regardless of era.
02 / Specs & Design
◎General5MOD.5
  • First Flight1949
  • Service Entry Year1950
  • Crew6
  • Primary RoleHeavy-lift military transport
  • In ServiceNo
◈Powerplant3MOD.3
  • Engine TypePratt & Whitney R-4360-63A Wasp Major
  • Number of Engines4
  • Power (each, turboprop)2,835 kW
▣Performance6MOD.6
  • Cruise Speed370.116 km/h
  • Top Speed489.197 km/h
  • Service Ceiling6,644.64 m
  • Maximum Range4,000 km
  • Range with Max Payload2,800 km
  • Takeoff Run2,000 m
◇Cargo & Capacity5MOD.5
  • Maximum Payload31,080 kg
  • Troop Capacity200
  • Paratroop Capacity200
  • Vehicle Capacity68,500 lb cargo or 200 troops
  • Rear Loading RampYes
◆Dimensions & Weights5MOD.5
  • Length39.624 m
  • Wingspan53 m
  • Height14.6 m
  • Empty Weight45,888.444 kg
  • Max Takeoff Weight86,180 kg
▤Production3MOD.3
  • Total Built448
  • Operators1
  • Variants5
⬢Service History4MOD.4
  • Retirement Year1974
  • Production Start1949
  • Production End1955
  • Operational StatusRetired
03 / History
SERVICE LIFESPANStill in Service
  1. 1945First deployment: Cold War
  2. 1950Production started
  3. 1955Production ended
76
years in service
5
years in production
448
units produced
1
countries operating
ⓘ The producing country still actively operates it.
04 / Conflicts
DOUGLAS C-124 GLOBEMASTER II · CONFLICTS SERVED IN50% win
Total Conflicts
2
Victories
1
Ongoing
0
Losses
0
ⓘ Shown only from conflicts recorded in our database.
05 / Operators
Operator Inventory1country · 235units
235active
📖 TERMS ON THIS PAGE1terms
A hinged rear fuselage section on military transport aircraft that lowers to enable direct loading/unloading of cargo or vehicles from the aircraft's tail.
These terms are listed automatically because they appear on this page.full encyclopedia →
📚 Sources
📖 ENCYCLOPEDIA Browse the Tactical Transports entry →