C-17 vs C-5 Galaxy: Payload, Range and Mission Compared
The C-5M Super Galaxy carries more weight and offers a much larger cargo compartment; the C-17 Globemaster III trades some capacity for a smaller crew, airdrop capability and access to shorter, narrower and more austere airfields. The Air Force keeps both because they solve different parts of the strategic-airlift problem.
This comparison uses current U.S. Air Force fact sheets. Runway, payload and range figures describe published reference conditions—not permission to plan a real mission without current approved data.
C-17 vs C-5 specifications
| Specification | C-17 Globemaster III | C-5M Super Galaxy |
|---|---|---|
| Primary role | Cargo and troop transport; strategic delivery, tactical airlift and airdrop | Outsize strategic cargo transport |
| Maximum cargo | 170,900 lb | 281,001 lb |
| Pallet positions | 18 | 36 |
| Cargo-compartment length | 88 ft | 143 ft 9 in |
| Cargo-compartment width | 18 ft | 19 ft |
| Cargo-compartment height | 12 ft 4 in | 13 ft 6 in |
| Maximum takeoff weight | 585,000 lb | 840,000 lb |
| Published basic crew | 3: pilot, copilot, loadmaster | 7: pilot, copilot, two flight engineers, three loadmasters |
| Current USAF inventory | 222 in April 2025 fact sheet | 52 C-5B/C/M in Air Force fact sheet |
Payload: the C-5M carries about 110,000 pounds more
The C-5M’s published maximum cargo load is 281,001 pounds, about 110,000 pounds more than the C-17’s 170,900-pound maximum payload. Its cargo compartment is also more than 55 feet longer and provides twice as many pallet positions.
That makes the C-5M the stronger choice when cargo weight, length or total volume exceeds the C-17’s envelope. Actual loadability still depends on dimensions, floor and axle loading, restraint, center of gravity and the route. A maximum-payload number alone never proves that a specific combination of vehicles fits.
Cargo access: two ends versus one
The C-5M can open both its nose and aft cargo doors. Full-width ramps allow simultaneous loading and unloading from both ends and support drive-through handling of long or oversized equipment.
The C-17 loads through a large aft ramp and door. Its floor converts between a flat surface for wheeled or tracked vehicles and rollers for pallets. The Air Force identifies the 69-ton M1 Abrams among the equipment the C-17 can accommodate, subject to qualified load planning.
Airfield access: the C-17’s defining advantage
The Air Force publishes a C-17 capability to take off and land on runways as short as 3,500 feet and 90 feet wide under the conditions behind that figure. High-lift devices, externally blown flaps and thrust reversers support short-field and austere operations. The aircraft can also back under its own power and use a three-point turn on a narrow runway.
The C-5M can operate from relatively short runways for an aircraft of its size, but its 247-foot length, 223-foot-class wingspan, 840,000-pound maximum takeoff weight and infrastructure needs make it a different airfield-planning problem. A dated GAO comparison used a 6,000-foot minimum reference for the C-5 versus 3,500 feet for the C-17. Real suitability depends on pavement strength, width, obstacles, weather, weight and current performance data.
Range: compare equal payload conditions
Range comparisons often become misleading because the payload assumptions differ. The Air Force lists these reference points:
- C-17: approximately 2,400 nautical miles with a 164,900-pound payload and an initial cruise altitude of 28,000 feet.
- C-5M: approximately 4,800 nautical miles with 120,000 pounds of cargo.
- C-5M at 281,001 pounds: 2,150 nautical miles, followed by an offload and a further 500-nautical-mile flight without refueling.
Both aircraft can refuel in flight. Neither maximum range nor maximum payload should be quoted without the accompanying conditions.
Crew and ground-support footprint
The C-17’s basic crew is three. The C-5M fact sheet lists seven: a pilot, copilot, two flight engineers and three loadmasters. Missions can add personnel or augment crews, but the published basic crews show the design difference.
The C-5M’s greater size and two-end loading capability can move more cargo per sortie, while the C-17’s smaller crew and forward-field design can make it more flexible near the destination. The most efficient choice depends on cargo, airfield, schedule, support and onward-movement requirements—not a single “better aircraft” score.
Airdrop and personnel missions
The C-17 was designed for tactical airlift and airdrop as well as strategic delivery. The Air Force publishes capacity for 102 troops or paratroopers and identifies airdrop as a core mission.
The C-5M fact sheet defines its primary function as outsize cargo transport. Its strength is moving very large loads over intercontinental distances, not replacing the C-17’s combination of strategic lift, airdrop and austere-field access.
Which aircraft should a mission use?
| Mission need | Usually favors | Why |
|---|---|---|
| Heaviest or longest outsize cargo | C-5M | 281,001-lb maximum cargo and much longer compartment |
| Twice the pallet positions | C-5M | 36 versus 18 |
| Short, narrow or austere destination | C-17 | Published 3,500-by-90-foot capability and backing |
| Paratroop or cargo airdrop | C-17 | Airdrop is a core published mission |
| Drive-through cargo handling | C-5M | Opening nose and aft doors |
Why the Air Force still needs both
The C-5M concentrates extraordinary capacity in each sortie. The C-17 provides less capacity but reaches a wider range of airfields and performs missions such as airdrop. In a deployment network, C-5Ms can move the largest loads between major hubs while C-17s can deliver substantial cargo farther forward. The exact routing is a planning decision, not a rigid rule.
Air Mobility Command stated in 2026 that Next Generation Airlift will eventually replace the aging C-5M and C-17 fleets. Until that capability is defined, acquired and fielded, the existing aircraft remain complementary rather than interchangeable.
For more detail, see the C-17 cargo-capacity guide, the official C-17 operating-cost rates, and the distinct C-5 vs C-17 vs C-130 comparison.
C-17 vs C-5 FAQ
Which carries more cargo?
The C-5M. Its published maximum cargo load is 281,001 pounds versus 170,900 pounds for the C-17.
Which has the larger cargo hold?
The C-5M. Its compartment is 143 feet 9 inches long, 19 feet wide and 13 feet 6 inches high. The C-17 compartment is 88 feet long, 18 feet wide and 12 feet 4 inches high.
Can both carry an M1 Abrams tank?
The Air Force fact sheets identify the M1 Abrams as transportable by both aircraft. The C-5M has much greater maximum cargo capacity, but every actual load requires current qualified planning.
Why not replace every C-5M mission with C-17s?
Some cargo is too heavy, long or voluminous for a C-17, and using multiple smaller sorties can reduce efficiency. Conversely, the C-17 can reach airfields and perform airdrop missions that define a different operational niche.
Official sources
- U.S. Air Force: C-17 Globemaster III fact sheet
- U.S. Air Force: C-5M Super Galaxy fact sheet
- GAO: comparison of C-5 and C-17 capabilities
- U.S. Air Force: Next Generation Airlift and strategic-airlift recapitalization
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