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Lockheed C-5 Galaxy


Strategic Heavy-Lifter Transport Aircraft (1970)


Aviation / Aerospace

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Jump-to: Specifications

The massive Lockheed C-5 Galaxy is the largest aircraft in service with the United States Air Force today - fulfilling the role of strategic heavy lifter in service.



Authored By: Staff Writer | Last Edited: 08/15/2018 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.
The United States Air Force (USAF) initiative that eventually begat the Lockheed C-5 "Galaxy" heavy-hauler was born from an effort to produce a long-range partner to operate alongside the existing USAF fleet of Lockheed C-141 "Starlifter" strategic transports. The complementary-minded C-5 was designed along the same strategic "heavy-hauling" (i.e. "out-sized") lines but became a much larger, more ambitious program which ultimately faced a variety of hurdles, both politically and technologically, before it became the robust, reliable platform seen today. While similar in mission scope to the C-141, the C-5 was to provide better performance and a longer-range, unrefueled cargo-hauling capability when ferrying dimensionally larger, heavier loads to points anywhere in the world - all this while operating from conventional airstrips and even unpaved landing zones.

The new aircraft arrived by way of the USAF's ever-evolving heavy-haul-minded programs of the 1960s that ultimately became the "Cargo Experimental - Heavy Logistics System" (CE-HLS). The service sought a four-engined product with a payload capability of 250,000lb flying over ranges of 3,000 miles without requiring aerial refueling. Because of the operating weights and power involved, it became obvious that a wholly-new fuel-efficient engine would be required. Additional qualities called for a fuselage with front and rear cargo access for "straight-through" loading / unloading.

The new proposal was drawn up in 1964 and some of the more traditional "big aircraft" American manufacturers responded like Boeing, Douglas, and Lockheed. These three passed into the design study phase and General Electric was commissioned to develop the engine. In the end, the Lockheed proposal won out over the others on cost despite authorities favoring the Boeing submission. The official announcement came in September of 1965 and the engines became the General Electric "TF39".

The Lockheed aircraft carried shoulder-mounted, swept-back wing mainplanes to which each held a pair of underslung engine nacelles towards their leading edges. The flightdeck was seated over a short, downward-sloped nose cone giving a commanding view of the ground ahead. The nosecone was hinged to open upwards allowing access to the hold within the body of the aircraft. The tail unit was raised aft of center mass to provide unrestricted access to the rear cargo area. The tail itself was arranged as a "T-style" assembly in which a single vertical fin supported very-high-mounted horizontal planes (these planes also swept-back). To round out the list of details, a multi-wheeled / multi-legged undercarriage configuration relying on new fewer than 28 wheels (!) was used to better balance the heavy aircraft on runways. The typical crew numbered seven to include three loadmasters and two flight engineers.

The cargo hold was designed to be large enough to accept a Sikorsky UH-60 type helicopter or similar up to the more modern Boeing V-22 Osprey systems. Beyond aircraft, the hold could also support all manner of cargo palettes and military vehicles giving the USAF a comprehensive heavy-lifter regardless of operating theater.

When introduced in 1970, the C-5 Galaxy became the largest aircraft in the world and remains one of the largest today (2016) - its dimensions include a wingspan of 222.8 feet, a length of 247 feet, and a height of 65 feet.

First-flight of a Galaxy was recorded on June 30th, 1968 and the aircraft was already proving heavier than initially planned. This added stresses to the wide-spanning wings which forced several modifications to their design. The expected payload capability, therefore, was decreased some. Beyond technical issues with such an expansive project, the inherently ambitious nature of the entire program ensured that the C-5 would become an expensive beast to develop and procure - the product indeed came under fire from Congress on several occasions during its development phase. Testing finally ended in 1969.

Ultimately the bloated program yielded some fruit in the arrival of the first production form - the "C-5A". Formal service introduction followed in June of 1970 with deliveries to the 437th Airlift Wing (Charleston AFB). At this time, Lockheed faced financial troubles that required government support simply to keep the C-5 program alive. In 1976 it was revealed that the wings, in an effort to address payload/range performance, were made too light in their design and proved prone to cracking so a new initiative was established to "re-wing" C-5As. Other welcomed changes included introduction of the TF39-GE-1C engines of 43,000lb thrust which increased the Maximum Take-Off Weight (MTOW). This work was completed from 1980 through 1987.
The "C-5B" was born from the revised A-model as an improved form and was born in 1982, arriving for service in 1986. Beyond the A-model introductions (including the wings), upgraded General Electric engines, updated avionics, and a revised undercarriage greeted the mark. A first-flight of a C-5B was recorded in September of 1985 and 50 total units were delivered from 1986 until 1989.

From the B-models came the "C-5C" which were technically recognized as C-5A(C) SCM = "Space Cargo Modified". As their name implied these were developed with increased internal volume in mind though only two of this mark were completed. The aircraft have served NASA with out-sized cargo delivery.

In 1998, the Galaxy fleet was modernized as a whole under the "Avionics Modernization Program" (AMP) and nearly all facets of the avionics fit were improved including cockpit displays and the autopilot system. Following in 2006 was a new program (RERP = "Reliability Enhancement & Re-engining Program") to address engines in an effort to extend the service life of the aircraft - the General Electric F138-GE-100 series of 50,000lb thrust each were introduced as a result. These units now promoted shorter take-off runs and a better climb-to-altitude rate while other facets of the large aircraft were further addressed to keep the mammoth machine flying for decades to come. The latest incarnation, based on this modernization program, has become the C-5M "Super Galaxy".

Beyond these produced variants were several unrealized forms - the "L-500" was a proposed civilian-minded model that came to naught, not only due to Lockheed's troubles but also because it managed little commercial interest. Another short-lived offshoot was a specially-modified C-5 to serve NASA's shuttle program as its space shuttle "carrier". The program eventually pursued the Boeing 747 for the role instead.

The C-5 series has served under the banners of Military Airlift Command / Air Mobility Command, Air Education & Training Command, the Air Force Reserve, and the Air National Guard. It has seen combat service (in a support role) since the Vietnam War (1955-1975), was critical to coalition operations in the 1991 Gulf War and in Yugoslavia later that decade, and - more recently - in serving coalition forces operating in Afghanistan. Beyond its obvious military value, the product has also contributed to multiple humanitarian, missions around the world.

Because of the project's infamous cost overruns, the C-5 Galaxy came to be known by some as the "Fantastic Ridiculous Economic Disaster" - or "FRED". The "Galaxy" name continued the Lockheed space-minded naming convention for its big aircraft products - "Starlifter", "Constellation", and so-forth.

C-5A models were produced from the period spanning 1968 to 1973 while C-5B models were manufactured from 1985 until 1989. Totals reached 131 of both systems, 81 A-models and 50 B-models. It is intended by the USAF that the C-5 family will continue to fly into 2040. The current (2016) inventory states 26 C-5A and 52 C-5B/C/M models in service.

August 2018 - Lockheed Martin delivered its final production C-5M (Modernized) Galaxy to the United States Air Force on August 2nd, 2018. The upgrades involved modernization of key systems, such as diagnostics, avionics and engines, to extend the service lives of these mammoth aircraft into the 2040s.

Specifications



Service Year
1970

Origin
United States national flag graphic
United States

Status
ACTIVE
In Active Service.
Crew
7

Production
131
UNITS


Lockheed / Lockheed-Martin - USA
National flag of the United States United States
(OPERATORS list includes past, present, and future operators when applicable)
Transport
General transport functionality to move supplies/cargo or personnel (including wounded and VIP) over range.


Length
247.1 ft
(75.31 m)
Width/Span
222.7 ft
(67.89 m)
Height
65.1 ft
(19.85 m)
Empty Wgt
379,989 lb
(172,360 kg)
MTOW
839,961 lb
(381,000 kg)
Wgt Diff
+459,972 lb
(+208,640 kg)
(Showcased structural values pertain to the Lockheed C-5B production variant)
Installed: 4 x General Electric TF39-GE-1C turbofans developing 43,000 lb of thrust each.
Max Speed
578 mph
(930 kph | 502 kts)
Ceiling
34,777 ft
(10,600 m | 7 mi)
Range
6,462 mi
(10,400 km | 19,261 nm)
Rate-of-Climb
1,800 ft/min
(549 m/min)


♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030


(Showcased performance specifications pertain to the Lockheed C-5B production variant. Compare this aircraft entry against any other in our database. View aircraft by powerplant type)
None.


C-5 "Galaxy" - Base Series Designation
C-5A - Initial production model series; 81 examples delivered; most re-winged in later years to counter structural weaknesses.
C-5B - Improved C-5A with improved automatic flight control system; redesigned and simplified undercarriage; new engines and wings for extended service life.
C-5C - Pair of modified C-5A models for satellite carriage (outsized space cargo operations); two examples completed.
C-5M "Super Galaxy" - Modernized Galaxy aircraft fleet.


Cockpit image of the Lockheed C-5 Galaxy
(Cockpit image represents the Lockheed C-5 production model)


General Assessment
Firepower  
Performance  
Survivability  
Versatility  
Impact  


Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
Overall Rating
The overall rating takes into account over 60 individual factors related to this aircraft entry.
32
Rating is out of a possible 100 points.
Relative Maximum Speed
Hi: 750mph
Lo: 375mph
This entry's maximum listed speed (578mph).

Graph average of 563 miles-per-hour.
City-to-City Ranges
NYC
 
  LON
LON
 
  PAR
PAR
 
  BER
BER
 
  MOS
MOS
 
  TOK
TOK
 
  SYD
SYD
 
  LAX
LAX
 
  NYC
Lockheed C-5B operational range when compared to distances between major cities (in KM).
Max Altitude Visualization
Small airplane graphic
Design Balance
The 3 qualities we look at for a balanced aircraft design are altitude, speed, and range.
Aviation Era Span
Pie graph section
Pie graph section
Showcasing era cross-over of this aircraft design.
Unit Production (131)
131
36183
44000
This entry's total production compared against the most-produced military and civilian aircraft types in history (Ilyushin IL-2 and Cessna 172, respectively).
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