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The Lockheed C-141 Starlifter & C-5 Galaxy

v1.0.9 / 01 apr 14 / greg goebel / public domain

* Two of the most prominent jet transport aircraft in US military service are the Lockheed "C-141 Starlifter" and its "big brother", the huge "C-5 Galaxy". This document provides a history and description of these two aircraft.

Lockheed C-141B Starlifter


[1] C-141A
[2] C-141B / NC-141A KAO / C-141B SOLL II / C-141C
[3] C-5A/B GALAXY
[4] RENEWING THE GALAXY: THE C-5M
[5] COMMENTS, SOURCES, & REVISION HISTORY

[1] C-141A

* In the 1950s, the US Air Force's Military Air Transport Service (MATS) was reliant on piston-engined cargolifters, such as the Douglas C-124 Globemaster. By the end of the decade, MATS brass had decided that they needed a more capable cargolifter, and in the spring of 1960 the USAF issued a request for proposals under the designation "Specific Operational Requirement 182 (SOR 182)". SOR 182 specified an aircraft with a cargo capacity of 27,200 kilograms (60,000 pounds) and a range of 6,480 kilometers (4,025 miles). Lockheed's proposal was selected, with an initial contract for five "development, test, and evaluation (DT&E)" aircraft awarded on 13 March 1961. The aircraft was given the designation "C-141 Starlifter".

The Starlifter incorporated ideas from Lockheed's earlier C-130 Hercules cargolifter, including a high wing; a loading ramp under the high tail; clamshell rear doors that could be opened in flight for airdrops; and main landing gear that retracted into fairings alongside the fuselage to ensure an unobstructed cargo hold. The Starlifter differed from the Hercules in having wings with a sweepback of 25 degrees and a tee tail, instead of straight wings and a conventional tail; and four Pratt & Whitney TF33-P-7 turbofans with 43.2 kN (9,525 kgp / 21,000 lbf) thrust each mounted in pods on underwing pylons, instead of turboprops mounted on the wing. There were typically five flight crew.

Initial flight of the Starlifter was on 17 December 1963. The first production "C-141A" was delivered to the USAF Military Airlift Command (MAC, successor to MATS) on 23 April 1965. A total of 284 C-141As was built through February 1968.

Once in service, the Starlifter immediately began daily shuttle flights from the continental US to Vietnam, carrying 138 passengers in rearward-facing seats, a configuration that the Air Force decided provided better safety in crashes; or up to ten standard 463L pallets with a total of 28,880 kilograms (62,700 pounds) of cargo. It returned with casualties: the aircraft could carry 80 litters with 23 medical attendants. A few Starlifters were modified to carry Minuteman ICBMs from the factory to operational bases.

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[2] C-141B / NC-141A KAO / C-141B SOLL II / C-141C

* In practice, MAC found that the Starlifter's cargo hold volume was small compared to its weight-lifting capability, meaning the aircraft often ran out of space well before it met its weight limit. To resolve this problem, in 1976 the USAF began a program to "stretch" the Starlifter with fuselage "plugs" in front of and behind the wing, increasing the length of the aircraft by 7.11 meters (23 feet 4 inches) and providing space for three more standard pallets, for a total of 13. The upgrade also involved the addition of a boom-refueling receptacle behind the cockpit.

The first "YC-141B" conversion performed its initial flight on 24 March 1977. A total of 270 "C-141B" conversions was performed through June 1982. The Air Force was very pleased with the conversion program, since it came through ahead of schedule and under budget, and gave MAC an increased airlift capacity equivalent to 90 more C-141As.

   LOCKHEED C-141B STARLIFTER:
   _____________________   _________________   _______________________
 
   spec                    metric              english
   _____________________   _________________   _______________________

   wingspan                48.74 meters        159 feet 11 inches
   wing area               300 sq_meters       3,228 sq_feet
   length                  51.29 meters        168 feet 4 inches
   height                  11.96 meters        39 feet 3 inches

   empty weight            677,200 kilograms   148,120 pounds
   loaded weight           155,600 kilograms   343,000 pounds

   max cruise speed        910 KPH             565 MPH / 490 KT
   normal cruise speed     800 KPH             495 MPH / 430 KT
   service ceiling         12,500 meters       41,000 feet
   loaded range            4,725 kilometers    2,935 MI / 2,555 NMI
   _____________________   _________________   _______________________

* Four "NC-141As" that were built as testbeds were not converted to C-141B standards. One of these, the "L-300" prototype for a commercial Starlifter that never went into production, was obtained by the US National Aeronautics & Space Administration (NASA) as a flying astronomical observatory and designated the "Kuiper Astronomical Observatory (KAO)".

NASA Kuiper Airborne Observatory

KAO was primarily intended to perform infrared observations of cosmic objects with a 91 centimeter (36 inch) telescope, mounted to perform observations out a hole in the fuselage. Such observations must be performed at high altitude, since the atmosphere absorbs infrared radiation. KAO went into service in 1974, and obtained many significant astronomical observations. The flying observatory was retired in 1995, as NASA was beginning work on a much more sophisticated flying observatory based on the Boeing 747SP jumbo jetliner, designated the "Stratospheric Observatory for Infrared Astronomy (SOFIA)". Retiring KAO freed up funds for the SOFIA effort.

* In 1994, the Air Force began a program to refit 13 C-141Bs to the "Special Operations Low-Level II (SOLL II)" standard, with a total program cost of $41 million USD. These aircraft were operated by the USAF in behalf of the US Special Operations Command, and included gear for low-level night flying, as well as defensive countermeasures.

The SOLL designation is a bit confusing; it only defined an operational mode, SOLL I being daylight low-level operations, and SOLL II being night low-level operations. In other words, SOLL II only described the aircraft mission, and did not imply "the second machine in the SOLL series of platforms". The SOLL II Starlifters were also sometimes referred to as "Special Operations Forces Improvement Modification (SOFI-Mod)" Starlifters.

The SOLL II Starlifter looked much like any other C-141B, but it could be recognized by three "knobs" on its chin. One knob was directly under the nose and was a turret for a Texas Instruments AN/AAQ-17 forward looking infra-red (FLIR) imager, which gave the aircraft the ability to "see in the dark". The FLIR imagery was displayed on a CRT at the navigator's station, and on an auxiliary display for the pilot. The navigator pointed the FLIR turret using a joystick. The FLIR turret could be removed for maintenance.

The other two knobs were for AN/ALE-40 chaff-flare dispensers, and were mounted on the "cheeks" of the aircraft. There were also chaff-flare dispensers in the landing-gear wheel wells and on the wingtips. In addition, the defensive countermeasures suite included an AN/AAR-44 infrared missile warning sensor fitted under the fuselage, and an AN/ALR-69 radar warning receiver with unobtrusive antennas tacked on to the nose and tail.

SOLL II Starlifter

The defensive countermeasures system could be set to an "automatic" mode to dispense chaff and flares without crew intervention. The amount of chaff and flares to be dispensed could be preprogrammed. The sensors also provided an audible warning to the crew through their headphones, with the crew dispensing chaff and flares themselves when the system was in "manual" mode. Even the loadmaster could activate the dispensers, as he or she often kept a "SAM (surface to air missile) watch" from the rear ramp.

The SOLL II Starlifter also included an enhanced suite of communications equipment and Global Positioning System (GPS) navigation gear. The enhancements of the SOLL II increased its weight by about 680 kilograms (1,500 pounds) compared to a "stock" C-141B. Crews were handpicked for night operations, which were conducted with night vision goggles (NVGs). All SOLL II Starlifter cockpit and exterior lighting was NVG-compatible. Additional crewmembers were included for missions of long duration or with high workload requirements. Passengers on SOLL II flights tended to find the low-level flight of the aircraft in pitch darkness, often in formation with another SOLL II aircraft, to be a little unnerving.

Lockheed C-141B Starlifter

* In the post-Vietnam era, the Starlifter was a major player in airlift operations to Haiti, Bosnia, Somalia, and Rwanda. It was used very heavily in the Gulf War in 1991. After the Gulf War, structural problems led to the imposition of flight restrictions, though these problems were quickly resolved by a comprehensive repair program. 63 Starlifters were also upgraded to the "C-141C" standard, with improved avionics, including GPS navigation gear and digital "glass" cockpits.

However, this update was just to provide a little incremental utility to stretch the type's service life a bit. The C-141 performed its final flight for the USAF's Air Mobility Command (AMC), the current incarnation of MATS and MAC, on 16 September 2004, with two aircraft sent off in a special ceremony from McGuire AFB in New Jersey to the "boneyard" at Davis-Monthan AFB in Arizona. Two AF Reserve squadrons continued to operate the type, but phased it out in the summer of 2006. The very last flight of the C-141C was on 6 May 2006, when a machine known as the "Hanoi Taxi" -- for its ferry flights of US prisoners from Hanoi in 1973 -- flew to Wright-Patterson AFB in Ohio for eventual display at the US Air Force Museum. It had performed almost 11,000 landings during its career as a C-141A, B, and C.

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[3] C-5A/B GALAXY

* In 1963, MATS issued a requirement for a "Cargo Experimental Heavy Logistics System (CX-HLS)" that specified a heavy long-range cargolifter to complement the Starlifter. The CX-HLS was to be capable of carrying 56,700 kilograms (125,000 pounds) of cargo over a range of 12,875 kilometers (8,000 miles).

In mid-1964, the USAF issued short-term contracts to Lockheed, Boeing, and McDonnell-Douglas for design studies of the CX-HLS, as well as to General Electric and Pratt & Whitney for design studies of new, highly efficient "high bypass ratio" turbofans to power the aircraft. GE won the engine competition in August 1963 with what would become the "TF39" turbofan, and Lockheed won the CX-HLS competition in October 1965 with their "L-500" design. The first Lockheed "C-5A Galaxy" flew on 30 June 1968. Deliveries began in 1970. A total of 81 C-5As was built.

The C-5A had the same overall configuration as the C-141, with high wing with a sweep of 25 degrees, four jet engines in pods on underwing pylons, a rear loading ramp, a high tee tail, and main landing gear retracting into fairings. However, it was massively scaled up, with the capability of lifting two main battle tanks or transporting 345 fully-equipped troops. The Galaxy was the largest operational aircraft in the world for 15 years, until it was surpassed by the Soviet Antonov An-124 Condor.

C-141 versus C-5

The C-5's nose hinged upward to allow "drive-through" access through the unobstructed cargo bay, which was pressurized and climate-conditioned. The dimensions of the hold were as follows:

   meters:  36.91 long (44.09 with ramps) x 4.11 high x 5.79 wide
   feet:    121 long (144.6 with ramps) x 13.5 high x 19 wide

The upraised nose cleared the cockpit, permitting the aircraft to be taxied with its nose open. The cockpit was placed at the front of an upper flight deck on top of the huge cargo hold, and accommodated a typical flight crew of six. The upper deck also included a 15-person crew-relief compartment with bunks in front of the wing, and a passenger compartment behind the wing with 73 rearward-facing seats.

The C-5A was powered by four General Electric TF39-GE-1 turbofans with 191.3 kN (19,500 kgp / 43,000 lbf) thrust each. All four engines had thrust reversers, and it seems the thrust reversers on the inboard engines could actually be activated while in flight. The aircraft had a four sets of main gear, each with two-axle bogies with two wheels in front and four in the rear, and a four-wheel nose gear. The landing gear could "kneel" to assist in loading cargoes, and featured a system to help land in crosswinds. The C-5A had a boom refueling capability from the start, as well as a computerized "Malfunction Detection, Analysis and Recording (MADAR)" diagnostic system that monitored 800 test points in flight or for ground servicing.

The C-5A proved its worth in the fall of 1973, in Operation NICKEL GRASS, the huge airlift to support Israel during the Yom Kippur war, with the big cargolifter carrying massive quantities of ammunition and weapons to assist Israeli forces. The Galaxy also performed reliable service in the last years of the Vietnam War, though one was lost on 4 April 1975 while trying to evacuate orphans from Saigon. 206 of the 382 people aboard were killed, many of them infants.

* The C-5A's design specifications had been very aggressive and hard to meet. The program did not go smoothly, and in fact the program is said to have coined the term "cost overrun". One of the long-term problems that resulted was that the aircraft did not live up to its fatigue-life specifications, with the wings having barely a quarter of the 30,000-hour lifetime specified. In 1975, Lockheed was awarded a contract to provide new wings to all surviving aircraft to increase the wing service life to the specified 30,000 hours. The first re-winged aircraft was delivered to the USAF in 1983, with the re-winging program complete by July 1987.

Lockheed C-5 Galaxy

* In 1982, the Air Force awarded Lockheed a contract for 50 "C-5Bs" that included the new wing; uprated TF39-GE-1C turbofans; improved alloys and fasteners; and improved avionics, including a MADAR II diagnostic system, Bendix weather radar with a color display, and a Delco triple-redundant inertial navigation system. The crosswind landing system of the C-5A, which had proven unreliable, was eliminated. Initial flight of the prototype was on 30 September 1985. Initial deliveries were in 1986 and all deliveries were completed in 1989.

   LOCKHEED C-5B GALAXY:
   _____________________   _________________   _______________________
 
   spec                    metric              english
   _____________________   _________________   _______________________

   wingspan                67.88 meters        222 feet 9 inches
   wing area               576 sq_meters       6,200 sq_feet
   length                  75.54 meters        247 feet 10 inches
   height                  19.85 meters        65 feet 2 inches

   empty weight            169,650 kilograms   374,000 pounds
   loaded weight           379,700 kilograms   837,000 pounds

   max cruise speed        910 KPH             565 MPH / 490 KT
   service ceiling         10,900 meters       35,750 feet
   fully-loaded range      5,525 kilometers    3,435 MI / 2,990 NMI
   _____________________   _________________   _______________________

* Two C-5s were fitted with a countermeasures suite much like that fitted to the SOLL II Starlifters, under a program designated PACER SNOW. Although some sources claim there were considerations for fitting the entire C-5 fleet with PACER SNOW gear, it didn't happen.

Two C-5As were modified for NASA to carry space shuttle payload bay cargoes, and were given the new designation of "C-5C". They were also known as the "Space Container Transport System (SCTS)", "Space Container Modifications (SCM)", "SCM Birds", or "Scum Birds". They were flown by Air Force crews but were under NASA's operational control, and the USAF had to ask NASA for permission to use them for non-NASA-related missions. They were also rumored to be used for ferrying top-secret cargoes to isolated bases for testing, but of course the government had no comment on such matters. With the end of the shuttle program, it appears these two machines are being returned to general Air Force service.

* The Galaxy, or "FRED (Fantastic Ridiculous Economic Disaster)" as it is known to its crews, has been a valuable asset for US military overseas deployments for three decades, and served with particular distinction in the Gulf War, lifting in a little more than two weeks more than the entire Berlin Airlift in 1949. One was lost in a crash at Ramstein Air Force Base in Germany on 29 August 1990. The accident was a misfortune, but at least it was the only loss of a transport during the Gulf War airlift, and only the fifth Galaxy lost during its entire operational history.

The C-5 has also served in later campaigns, up to and including the US occupation of Iraq. One was hit by what appears to have been a shoulder-fired SAM while leaving Baghdad International Airport on 8 January 2004. The transport's number four engine exploded, but the crew managed to get the machine turned back around and down onto the runway with no casualties.

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[4] RENEWING THE GALAXY: THE C-5M

* As of 2000, the AMC operated 126 C-5s, including 74 C-5As, 50 C-5Bs, and two C-5Cs. The C-5s represent an important asset that has a lot of value left in it. None of the C-5s in operational service are even halfway to their maximum airframe lives. The FRED had an excellent safety record, but its reliability left much to be desired, with a poor mission availability rate.

Lockheed C-5 Galaxy

A set of upgrades have been or are being implemented to keep the C-5 flying. The initial phase, the $500 million USD "Avionics Modernization Program (AMP)", began in 1999, with the first C-5 fitted with an AMP upgrade, consisting of a Honeywell "traffic alert and collision avoidance system (TCAS)", returned to Air Force service in August 2000. AMP featured installation of the Honeywell TCAS, with its own dedicated cockpit display.

That led to the much more comprehensive second phase AMP update, in which the TCAS was an integrated part of the new cockpit system, which features a digital flight-control system; a state-of-the-art communications and navigation suite, with satellite links and a GPS receiver; an enhanced ground proximity warning system; an ARINC-standard data bus; and seven 15 x 20 centimeter (6 x 8 inch) color flat-panel displays, with six for the pilot and copilot and one for the flight engineer. The new scheme is built around Honeywell Versatile Integrated Avionics (VIA) processors. The Honeywell flight-management system permits electronic upload of preprepared flight plans and can store up to 200 navigation waypoints, compared to 10 in the old system. According to Lockheed Martin, which implemented the AMP program, all the new equipment was based on commercially-available products.

The first full AMP upgrade was completed in late 2004, with the last of 79 C-5s upgraded to the spec redelivered in the spring of 2012. The full AMP upgrade gives the C-5 a flight deck equivalent to a state-of-the-art commercial airliner and will allow the cargolifter to meet Global Air Traffic Management standards anywhere in the world.

The third phase is to update AMP machines with new engines under the $7 billion USD "Reliability Enhancement & Reengining Program (RERP)", which is replacing the current GE TF39 turbofan engines with modern GE CF6-80C2 turbofans. The CF6-80C2 is well-proven, being used on the Boeing 747 and 767, and normally offers 266.9 kN (27,210 kgp / 60,000 lbf) thrust each, though the engines are derated to 222.4 kN (22,675 kgp / 50,000 lbf) thrust since the airframe can't handle the additional power. Derating the engines is not a loss, however, since it improves engine reliability, which is already very high. Time between overhauls per engine is expected to increase from 2,000 hours to 10,000 hours. The new engines are also more fuel efficient, permitting longer flights without stopovers or tanker support.

Lockheed Martin is also implementing this program, with re-engining begun in 2003 and the initial flight of the first re-engined C-5 on 19 June 2006, with USAF Lieutenant Colonel Todd Markwald in command. After the flight, Markwald commented: "The aircraft felt like it was made for this engine more so than for the old ones."

Lockheed Martin chose the GE engine over the Pratt & Whitney PW4650 and the Rolls-Royce Trent 500. GE will perform off-wing maintenance on the engines for the USAF. RERP also involves a few structural enhancements to deal with a new pattern of airframe loads; a new Hamilton Sundstrand auxiliary power unit (APU); new engine pylons; improvements to the aircraft's antiskid landing gear and climate-conditioning systems; and, significantly, fit of the "Large Aircraft Infrared Countermeasures (LAIRCM)" defensive system. LAIRCM features a missile-warning system and a laser turret to "dazzle" heat-seeking missiles; it allows the C-5M to operate out of airfields in hot combat zones. The renewed C-5s, redesignated the "C-5M Super Galaxy", have much improved performance, with over twice the top payload capacity and a faster climb rate, and the new engines are significantly quieter as well.

The program has not gone entirely smoothly and the Air Force didn't g1ve the green light for RERP production until 2009. By early 2014, 16 C-5Ms had been redelivered, with formal introduction to service at that time. Under the plan, 12 to 15 C-5s will be upgraded every year. Due to funding cutbacks, only 52 of the C-5A fleet will be updated to C-5M standard to keep them in service until at least 2040, with the last refurbished machine to be delivered in 2017; the rest of the C-5As will be retired.

As a follow-up, Lockheed Martin has investigated enhancements to increase the fuel efficiency of the C-5, an important consideration in an era of costly fuel. The enhancements include improved flight surfaces; better pressurization seals to reduce demand for engine bleed air; streamlining of defensive countermeasures modules; and possibly 1.8 meter (6 foot) tall winglets. Fuel savings would be on the order of 3%. There is no commitment to these fixes at present, but they are clearly attractive. Studies are already underway for a much more fuel-efficient replacement.

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[5] COMMENTS, SOURCES, & REVISION HISTORY

* During the late 1960s and early 1970s, I used to see C-141s coming into Fairchild Air Force base near Spokane, Washington, on an occasional basis. Some claim it is an ugly aircraft, but I've always found it somewhat elegant myself. As far as the C-5 goes, I have a memory of one flying over Spokane in the same timeframe, with the thing so huge that it appeared to float in the sky like an airship.

In 1973, when I was stationed at Fort Hood, Texas, I also watched C-5s swallowing up M-60 tanks as part of the NICKEL GRASS airlift to Israel during the Yom Kippur War. It is an interesting memory to have observed history in progress, though the details have largely faded away. As I learned much later, the load I observed was unusual; tanks were only carried as something of a test, since the Israelis really needed spares and particularly ammunition.

Lockheed C-5 Galaxy

* Sources include:

Some details on the C-5 were also obtained from a web document by Jason Hodgkiss, as well as THE AVIATION ZONE website, which is refreshingly dedicated to "big lifters" instead of the usual assortment of fighters and bombers more commonly favored on the web.

* Revision history:

   v1.0   / 01 jul 01 
   v1.0.1 / 01 jun 02 / Review & polish.
   v1.0.2 / 01 jun 04 / Review & polish.
   v1.0.3 / 01 jul 04 / Review & polish.
   v1.0.4 / 01 aug 06 / C-5M modernization program details.
   v1.0.5 / 01 jan 07 / Review & polish.
   v1.0.6 / 01 jan 09 / Review & polish.
   v1.0.7 / 01 apr 10 / Minor corrections on RERP.
   v1.0.8 / 01 may 12 / Review & polish.
   v1.0.9 / 01 apr 14 / Review & polish.
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