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Lockheed C-5M Super Galaxy
Category | Strategic Heavy Transport Aircraft | ||||||||
|---|---|---|---|---|---|---|---|---|---|
Origin | United States (Lockheed Martin) | ||||||||
First Flight and Entry into Service Year | First C-5 Galaxy Flight: 30 June 1968 C-5M Super Galaxy Entry into Service: 2009 | ||||||||
Number Produced | Total C-5 Galaxy Series: 131 C-5M Modernization: Approximately 50 | ||||||||
Engine and Power System | 4 × General Electric CF6-80C2L1F turbofan engines | ||||||||
Users | United States Air Force (USAF) | ||||||||
Dimensions | Length: 75.5 metres Wingspan: 67.9 metres Height: 19.8 metres | ||||||||
Weights | Empty Weight: Approximately 172,000 kg Maximum Takeoff Weight: 381,000 kg Payload Capacity: 129,000 kg | ||||||||
Performance | Maximum Speed: Mach 0.77 (approximately 917 km/h) Range (with maximum load): 4,440 km Range (unrefuelled): Approximately 11,000 km Service Ceiling: 10,600 metres (35,000 ft) | ||||||||
Lockheed C-5M Super Galaxy is a critical component of the United States Air Force’s (USAF) strategic airlift capability. As a modernized version of the original C-5 Galaxy, the C-5M plays a vital role in the intercontinental transport of heavy and oversized military equipment. This aircraft is a key asset in supporting the United States’ global military operations and humanitarian missions.

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The initial version of the C-5 Galaxy was developed in the 1960s and entered service in the 1970s. Over time, performance issues and rising maintenance costs necessitated its modernization. In this context, the Lockheed Martin-led C-5M Super Galaxy program aimed to extend the service life of the C-5 fleet into the 2040s. The program encompasses three key modernization areas:
The technical specifications of the C-5M Super Galaxy make it one of the largest and most capable military transport aircraft in the world:
The C-5M is used for global military operations, humanitarian missions, and strategic logistical support. The aircraft’s front and rear cargo doors can be opened, enabling rapid loading and unloading of vehicles and cargo. Additionally, its “kneeling” feature facilitates easier loading operations.
The modernized engines of the C-5M have significantly improved the aircraft’s performance:

Generated by artificial intelligence.
The United States Air Force operates approximately 50 C-5M Super Galaxy aircraft. These aircraft primarily serve under Air Mobility Command (AMC) and Air Force Reserve Command (AFRC).
The C-5M, alongside aircraft such as the Antonov An-124 and An-225, ranks among the world’s largest and most powerful military transport aircraft. Strategically, it is a cornerstone of the United States’ global military reach. It has played a critical role in operations across the Middle East, Europe and Asia. Over its more than 50 years of service, the C-5M has proven to be an indispensable asset in strategic airlift operations.
"C-5 A/B/C Galaxy and C-5M Super Galaxy > Air Mobility Command > Display". AMC.af.mil. Accessed April 21, 2025.
"C-5M Super Galaxy." Air Force. Fact Sheet Display. AF.mil. Accessed April 21, 2025.
"Göklerdeki 50. yılında C-5 Galaxy | DefenceTurk". Defenceturk.net. Accessed April 21, 2025.
Lockheed Martin. "C-5M Super Galaxy Redefining Strategic Airlift - Lockheed Martin." Accessed April 21, 2025.https://www.lockheedmartin.com/content/dam/lockheed-martin/aero/documents/c5/c5_product_card_m11-1132343a.pdf

Lockheed C-5M Super Galaxy
Category | Strategic Heavy Transport Aircraft | ||||||||
|---|---|---|---|---|---|---|---|---|---|
Origin | United States (Lockheed Martin) | ||||||||
First Flight and Entry into Service Year | First C-5 Galaxy Flight: 30 June 1968 C-5M Super Galaxy Entry into Service: 2009 | ||||||||
Number Produced | Total C-5 Galaxy Series: 131 C-5M Modernization: Approximately 50 | ||||||||
Engine and Power System | 4 × General Electric CF6-80C2L1F turbofan engines | ||||||||
Users | United States Air Force (USAF) | ||||||||
Dimensions | Length: 75.5 metres Wingspan: 67.9 metres Height: 19.8 metres | ||||||||
Weights | Empty Weight: Approximately 172,000 kg Maximum Takeoff Weight: 381,000 kg Payload Capacity: 129,000 kg | ||||||||
Performance | Maximum Speed: Mach 0.77 (approximately 917 km/h) Range (with maximum load): 4,440 km Range (unrefuelled): Approximately 11,000 km Service Ceiling: 10,600 metres (35,000 ft) | ||||||||
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Design and Development Process: The Need for Modernization
Technical Specifications
Operational Use: Global Missions
Impact of Modernization: Performance Enhancements
Active Fleets
Historical and Strategic Significance: Global Reach