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C-130 Hercules vs C-17 Globemaster III

C-130 Hercules vs C-17 Globemaster III at a glance — top speed 593 vs 930 km/h, range 3,800 vs 4,480 km, max takeoff weight 70,307 vs 259,460 kg, built 2,500 vs 279 units.

Specifications
C-130 Hercules C-17 Globemaster III
Origin country 🇺🇸 United States 🇺🇸 United States
Category Military Transport Aircraft Military Transport Aircraft
Manufacturer Lockheed McDonnell Douglas
First flight 23 August 1954 15 September 1991
Year introduced 1956 1993
Number produced 2500 units 279 units
Average unit price $68 million $340 million
Wing area 162.0 m² 353.0 m²
Wingspan 40.4 m 51.8 m
Height 11.7 m 16.8 m
Length 29.8 m 53.0 m
Maximum speed 593 km/h 930 km/h
Operational range 3,800 km 4,480 km
Service ceiling 10,058 m 13,715 m
Max. takeoff weight 70,307 kg 259,460 kg
Empty weight 35,800 kg 122,000 kg
Total thrust 4 x 3,661 kW 4 x 18,909 kgf
Performance Radar Chart

Detailed Comparison

The USAF airlift doctrine relies on a tiered system where the C-17 Globemaster III executes inter-theater outsize cargo delivery, while the C-130 Hercules handles intra-theater tactical distribution. Procured at $340 million per unit, the C-17 operates as a strategic asset bridging the gap between the massive C-5 Galaxy and the tactical C-130. The $68 million C-130, with a production run exceeding 2,500 units since 1954, serves as the utility transport for 70 nations.

Development and Design

Lockheed engineered the C-130 in the 1950s around four Allison T56 turboprops and a high-wing, low-stance fuselage to enable rolling cargo transfer on unpaved dirt strips. Its straight-wing design prioritizes low-speed handling over transit speed. McDonnell Douglas developed the C-17 in the 1980s to bypass the traditional hub-and-spoke airlift model. By employing externally blown flaps routed through Pratt & Whitney F117 turbofans, engineers gave the C-17 the payload capacity of a strategic airlifter with the short-field landing profile of a tactical transport, allowing direct delivery from the continental US to forward operating bases.

Specifications and Performances

The performance delta between the two platforms dictates their operational boundaries:

  • Speed and Range: The C-17 cruises at 930 km/h with a 4,480 km range, enabling trans-oceanic delivery. The C-130 is restricted to 593 km/h and a 3,800 km range, confining it to regional operations.
  • Payload Capacity: With a 259,460 kg maximum takeoff weight, the C-17 carries 77,500 kg (accommodating an M1 Abrams tank). The C-130 maxes out at 70,307 kg MTOW with a 19,000 kg payload limit.
  • Runway Requirements: The C-130 lifts off in 1,093 meters and lands on unimproved dirt. The C-17 requires 2,500 meters at maximum weight and demands higher Load Classification Number (LCN) surfaces to prevent pavement degradation.

Deployment and usage

During Operation Enduring Freedom, the USAF utilized the C-17 to fly directly from Ramstein Air Base to drop zones in northern Afghanistan, executing 15-hour missions with combat loads. However, the aircraft's footprint limits its access to light runways. The C-130 executes the final tactical mile. At Khe Sanh in 1968 and at forward operating bases in Iraq, C-130s landed on pierced steel planking, dirt, and gravel. Furthermore, the C-130 airframe serves as a modular platform, executing electronic attack (EC-130H), special operations refueling (MC-130), and close air support (AC-130) missions that the single-role C-17 does not perform.

Conclusion

For expeditionary forces requiring outsize armor and rapid inter-theater transit, the C-17 is the required asset. It is the sole western transport that delivers 77,500 kg payloads directly to forward airfields. However, the C-130 out-performs the C-17 in sustained intra-theater logistics and multi-mission adaptability. When operations require resupply into unimproved, low-load-bearing dirt strips or demand specialized gunship and electronic warfare configurations, the C-130 is the mandatory airframe. The C-17 controls heavy inter-theater projection, while the C-130 dictates tactical distribution in austere environments.

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Frequently Asked Questions

Which is faster, the C-130 Hercules or C-17 Globemaster III?
The C-17 Globemaster III is faster with a maximum speed of 930 km/h compared to the C-130 Hercules's 593 km/h, a difference of 337 km/h.
Which has longer range, the C-130 Hercules or C-17 Globemaster III?
The C-17 Globemaster III has a longer range at 4,480 km compared to the C-130 Hercules's 3,800 km.
Which can fly higher, the C-130 Hercules or C-17 Globemaster III?
The C-17 Globemaster III has a higher service ceiling at 13,715 meters (44,996 ft) compared to the C-130 Hercules's 10,058 meters (32,998 ft).
Which is heavier, the C-130 Hercules or C-17 Globemaster III?
The C-17 Globemaster III has a higher maximum takeoff weight at 259,460 kg compared to the C-130 Hercules's 70,307 kg.
Which is larger, the C-130 Hercules or C-17 Globemaster III?
The C-17 Globemaster III is longer at 53.0 meters compared to the C-130 Hercules's 29.8 meters.
Which is more expensive, the C-130 Hercules or C-17 Globemaster III?
The C-17 Globemaster III is more expensive at approximately $340 million per unit compared to the C-130 Hercules at $68 million.
Which entered service first, the C-130 Hercules or C-17 Globemaster III?
The C-130 Hercules entered service first in 1956, 37 years before the C-17 Globemaster III which entered service in 1993.
Which has been built in greater numbers, the C-130 Hercules or C-17 Globemaster III?
The C-130 Hercules has been produced in greater numbers with 2,500 units compared to 279 units of the C-17 Globemaster III.