ARMSNET
Military Equipment Database
Initializing 0%

C-5M Super Galaxy

C-5M Super Galaxy

Military Transport Aircrafts
Spotted an error? Sign in to suggest an edit.
Basic Information
Name
C-5M Super Galaxy
Designation
C-5M Super Galaxy
Alternate Designation
C-5 RERP
Equipment Type
Military Transport Aircrafts
Manufacturer
Lockheed Martin
Date of Introduction
2011
Description

The AMP package installation on US Air Force C-5s started in June 2004 and is expected to last several years. In October 2004, the first C-5 AMP was delivered to Lockheed-Martin to undergo RERP upgrade modifications. The RERP program will see the first C-5 aircraft taking to the air in October 2005 or later for testing powered by four fuel efficient F138-GE-100 engines (a CF6-80C2 derivative). The test program is expected to complete in 2007. The C-5 aircraft that had received both AMP and RERP modifications will be re-designated C-5M Super Galaxy. As of early 2006, the USAF plans call for 112 C-5A/B aircraft to undergo C-5M modernization program through 2020. The program was scoped for only 52 C-5M delivered by August 2018 and to remain in active duty in the 2040s. The C-5A/B Reliability Enhancement and Re-engining Program (RERP) includes new F103 engines (a derivative of proven CF6 commercial engines), pylons and auxiliary power units, with upgrades to aircraft skin and frame, landing gear and the pressurization system. Overall RERP includes more than 70 system and equipment improvements. AMP and RERP programs will restore C-5's maintainability and reliability, maintain structural and system integrity, reduce overall ownership costs and increase operational capability well into the 21st century. Overall, the C-5 upgraded aircraft fleet mission capable rate would represent at least 75 percent. The US Air Force (USAF) long-term goal is to keep the C-5 strategic transport aircraft fleet viable for the next 40 years. In actual facts, AMP program is the first phase of such effort, while RERP program will act as the second phase leading to the fully upgraded C-5 aircraft.

Air & Air Defense Specifications
Crew 7
Max Speed 921.6 km/h
Range 3980.0 km
Wingspan 67.90 m
Overview (Deagel)
Group Military Transport Aircrafts
Status Active
Also Known As C-5 RERP
Origin United States of America
Contractor Lockheed Martin
Initial Operational Capability (IOC) 2011
First Flight September 19, 2010
Total Production ?
Development Cost USD $1.2 billion
Specifications (Deagel)
Crew 7
Number of Engines 4
Service Life Flight Hours 45000
Dimensions — Height 19.8 meter
Dimensions — Length 75.3 meter
Dimensions — Wingspan 67.9 meter
Mass — Cargo 122,500 kilogram
Mass — Max Takeoff Thrust 290,000 pound
Mass — Max Takeoff Weight 381 ton
Performance — Max Range 3,980 kilometer
Speed — Top Speed at High Altitude 256 mps
Gear (Deagel)
Item 1 Turbofan Engines: F138-GE-100 (4)
Variants
Variant 1 C-5 Galaxy
Variant 2 C-5M Super Galaxy
Details
Country of Origin United States
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
75.3 m
Width
67.9 m
Height
19.8 m
Weight
381000 kg
Operators (1)
United States
Something went wrong. Please reload the page. Reload