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Douglas C-124 Globemaster II


Heavy-Lift Transport Aircraft


United States | 1950



"The Globemaster II was a direct post-war design development of the World War 2-era C-74 Globemaster I."



Authored By: Staff Writer | Last Edited: 06/18/2017 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site; No A.I. was used in the generation of this content.
With the close of World War 2 and the accompanying Berlin Airlift, the United States military saw a need to replace its aged C-74 "Globemaster I" systems with a newer and more capable platform. The C-124 was put forth as a product of the Douglas Aviation Company and accepted as the "Globemaster II". From 1950 to 1974, the C-124 served a pivotal role through two major conflicts in Korea and Vietnam and several smaller engagements along the way. As a cargo hauler, it was the best available at what it was asked to do. And what it was asked it do, the Globemaster II did extremely well.

Visually the C-124 was characterized by its enlarged frontal fuselage and low-mounted wings, each fitted with two engines. Cargo access was accomplished through a front twin door opening (sometimes called a clamshell) just underneath the flight deck. The forward cargo bay opening was also featured with a powered lift while an additional cargo entry/exit position was made available on the aft underside. A single vertical tail surface was mounted atop the empennage. Crew accommodations amounted to six personnel. Power was supplied from no fewer than 4 x Pratt & Whitney R-4360 piston engines of the "Wasp Major" type - powerful engines generating some 3,800 horsepower apiece.

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The C-124 saw extensive action in the Korean War and into the Vietnam conflict. the system was quite capable of accomplishing any wartime feat that including the transportation of armor, artillery pieces, construction/engineering equipment, general supplies and ballistic missiles. The C-124 was also versatile enough as a passenger transport or medical patient mover, moving some 200 soldiers or 127 wounded at a time. In the end, the C-124 was an excellent logistical piece for the American military and its many years of service proved just that.

Operating branches of the C-124 system included the United States Air Force (SAC), the Air National Guard and the Military Air Transport Service. USAF C-124's were officially retired in 1974 and, in all, some near-450 examples were produced. Visitors to the United States Air Force Museum are treated to an indoor static display of an open C-124 (s/n 51-0135) to which they can walk up into the cargo hold of the aircraft.

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Cockpit
While traditional jobs involve workstations, office desks, or cubicles, aircraft provide operators with their own unique, ever-changing view of the world below.
Cockpit image
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Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Douglas C-124 Globemaster II Heavy-Lift Transport Aircraft.
4 x Pratt & Whitney R-4360 Wasp Major radial engines delivering 3,800hp each.
Propulsion
323 mph
520 kph | 281 kts
Max Speed
32,808 ft
10,000 m | 6 miles
Service Ceiling
2,175 miles
3,500 km | 1,890 nm
Operational Range
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).
NYC
 
  LON
LON
 
  PAR
PAR
 
  BER
BER
 
  MOS
MOS
 
  TOK
TOK
 
  SYD
SYD
 
  LAX
LAX
 
  NYC
Structure
The nose-to-tail, wingtip-to-wingtip physical qualities of the Douglas C-124 Globemaster II Heavy-Lift Transport Aircraft.
6
(MANNED)
Crew
131.2 ft
40.00 m
O/A Length
174.1 ft
(53.06 m)
O/A Width
48.2 ft
(14.70 m)
O/A Height
101,413 lb
(46,000 kg)
Empty Weight
194,007 lb
(88,000 kg)
MTOW
Design Balance
The three qualities reflected below are altitude, speed, and range. The more full the box, the more balanced the design.
RANGE
ALT
SPEED
Variants
Notable series variants as part of the Douglas C-124 Globemaster II family line.
C-74 - Globemaster I model series on which the C-124 was based on.
C-124 - Base Series Designation based on the C-74 Globemaster I design of World War 2.
C-124A - Second Production Variant
C-124C - Third production Variant; improved engines; radar fitted into new nose protuberance; specialized de-icing features implemented.
Operators
Global customers who have evaluated and/or operated the Douglas C-124 Globemaster II. Nations are displayed by flag, each linked to their respective national aircraft listing.

Total Production: 448 Units

Contractor(s): Douglas Aircraft - USA
National flag of the United States

[ United States ]
Relative Max Speed
Hi: 400mph
Lo: 200mph
Aircraft Max Listed Speed (323mph).

Graph Average of 300 MPH.
Era Crossover
Pie graph section
Showcasing Aircraft Era Crossover (if any)
Max Alt Visualization
Small airplane graphic
Production Comparison
448
36183
44000
Entry compared against Ilyushin IL-2 (military) and Cessna 172 (civilian) total production.
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Aviation Timeline
EarlyYrs
WWI
Interwar
WWII
ColdWar
Postwar
Modern
Future
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Mission Roles
Some designs are single-minded in their approach while others offer a more versatile solution to airborne requirements.
TRANSPORT
Recognition
Some designs stand the test of time while others are doomed to never advance beyond the drawing board; let history be their judge.
Going Further...
The Douglas C-124 Globemaster II Heavy-Lift Transport Aircraft appears in the following collections:
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