GlobalMilitary.net Open-source military intelligence Updated daily

C-17 Globemaster III vs C-5 Galaxy

C-17 Globemaster III vs C-5 Galaxy at a glance — top speed 930 vs 932 km/h, range 4,480 vs 8,900 km, max takeoff weight 259,460 vs 381,017 kg, built 279 vs 131 units.

Lockheed C-5 Galaxy military transport aircraft side profile drawing
🇺🇸 C-5 Galaxy
Specifications
C-17 Globemaster III C-5 Galaxy
Origin country 🇺🇸 United States 🇺🇸 United States
Category Military Transport Aircraft Military Transport Aircraft
Manufacturer McDonnell Douglas Lockheed
First flight 15 September 1991 30 June 1968
Year introduced 1993 1971
Number produced 279 units 131 units
Average unit price $340 million $168 million
Wing area 353.0 m² 576.0 m²
Wingspan 51.8 m 67.9 m
Height 16.8 m 19.8 m
Length 53.0 m 75.3 m
Maximum speed 930 km/h 932 km/h
Operational range 4,480 km 8,900 km
Service ceiling 13,715 m 10,600 m
Max. takeoff weight 259,460 kg 381,017 kg
Empty weight 122,000 kg 172,365 kg
Total thrust 4 x 18,909 kgf 4 x 19,674 kgf
Performance Radar Chart

Detailed Comparison

The USAF airlift doctrine distributes its logistics between the Lockheed C-5 Galaxy, tasked with outsized, intercontinental hauling, and the Boeing C-17 Globemaster III, tasked with bypassing theater hubs to transport strategic cargo directly to austere tactical airfields. The C-5 maximizes absolute volume and payload, while the C-17 limits raw lift capacity to achieve high sortie generation rates and rough-field integration.

Development and Design

Lockheed’s C-5 emerged from the 1963 CX-HLC requirement to out-lift the C-141. Early development was marred by severe weight growth, wing structural failures that initially restricted fleet load capacity to 80%, and a congressional investigation over $1 billion in cost overruns. The USAF eventually funded a re-winging program for the C-5A fleet and later initiated the Reliability Enhancement and Re-engining Program (RERP) to upgrade the aircraft to the C-5M standard with General Electric CF6 engines. Conversely, McDonnell Douglas developed the C-17 in the 1980s to directly replace the C-141 while matching the tactical utility of the C-130. The C-17 integrates an internally blown flap system and fully articulated landing gear, allowing a 259,460 kg aircraft to operate from unpaved, forward-deployed airstrips.

Specifications and Performances

Performance metrics dictate their doctrinal roles. The C-5 dwarfs the C-17 in raw capacity, with a maximum takeoff weight of 381,017 kg and a 127,459 kg payload limit. It can accommodate two M1 Abrams tanks or an armored vehicle-launched bridge. The C-5's 8,900 km range enables non-stop intercontinental transits without aerial refueling.

In contrast, the C-17 trades mass for accessibility:

  • Payload caps at 77,519 kg, restricting it to a single M1 Abrams tank per flight.
  • Unrefueled range sits at 4,480 km, requiring tanker support for transoceanic deployments.
  • Takeoffs require 2,500 m of runway, but the aircraft routinely lands on 1,000 m dirt strips using Pratt & Whitney F117 thrust reversers.

Deployment and usage

The C-5 proved its intercontinental utility during the 1973 Yom Kippur War (Operation Nickel Grass) and the 1991 Gulf War, moving outsized cargo that no other allied airframe could accommodate. However, its historical mission capable rates frequently hovered below 60%, anchoring the aircraft to well-paved, established logistical hubs. The C-17 altered tactical airlift doctrine during Operations Enduring Freedom and Iraqi Freedom. By flying armored vehicles directly into forward operating bases like Bagram or dirt strips in northern Iraq, the C-17 eliminated the need to transload cargo onto C-130s. This reliability drove a 279-unit production run and secured exports to Australia, Canada, India, Qatar, and the UK, whereas the C-5 remains strictly a USAF asset.

Conclusion

The C-17 Globemaster III dictates the current tempo of US and allied logistics. While the C-5 remains the only solution for rapidly projecting massed heavy armor and outsized engineering equipment across oceans, its utility is tethered to major hubs and hampered by heavy maintenance demands. The C-17’s ability to bypass intermediate staging bases and transport strategic payloads directly into contested, austere environments makes it the more operationally relevant platform for modern, distributed warfare.

Change comparison vs

Frequently Asked Questions

Which is faster, the C-17 Globemaster III or C-5 Galaxy?
The C-5 Galaxy is faster with a maximum speed of 932 km/h compared to the C-17 Globemaster III's 930 km/h, a difference of 2 km/h.
Which has longer range, the C-17 Globemaster III or C-5 Galaxy?
The C-5 Galaxy has a longer range at 8,900 km compared to the C-17 Globemaster III's 4,480 km.
Which can fly higher, the C-17 Globemaster III or C-5 Galaxy?
The C-17 Globemaster III has a higher service ceiling at 13,715 meters (44,996 ft) compared to the C-5 Galaxy's 10,600 meters (34,776 ft).
Which is heavier, the C-17 Globemaster III or C-5 Galaxy?
The C-5 Galaxy has a higher maximum takeoff weight at 381,017 kg compared to the C-17 Globemaster III's 259,460 kg.
Which is larger, the C-17 Globemaster III or C-5 Galaxy?
The C-5 Galaxy is longer at 75.3 meters compared to the C-17 Globemaster III's 53.0 meters.
Which is more expensive, the C-17 Globemaster III or C-5 Galaxy?
The C-17 Globemaster III is more expensive at approximately $340 million per unit compared to the C-5 Galaxy at $168 million.
Which entered service first, the C-17 Globemaster III or C-5 Galaxy?
The C-5 Galaxy entered service first in 1971, 22 years before the C-17 Globemaster III which entered service in 1993.
Which has been built in greater numbers, the C-17 Globemaster III or C-5 Galaxy?
The C-17 Globemaster III has been produced in greater numbers with 279 units compared to 131 units of the C-5 Galaxy.