The
Boeing KC-135
Stratotanker was the first jet powered
aerial refueling tanker of the US Air
Force, replacing the
KC-97
Stratotanker. Similar in design to the later and enlarged
Boeing 707 airliner, it was initially
tasked to refuel strategic bombers, but was used extensively in the
Vietnam war and later conflicts such as
Desert Storm to extend the range and
endurance of both Air Force and Navy tactical fighters and
bombers.
Serving with the
United States
Air Force since 1957, it is one of just six military aircraft
with over 50 years of continuous service with the original service
along with the
Tupolev Tu-95, the
C-130 Hercules, the
B-52 Stratofortress, and the
Lockheed U-2. Supplemented by the larger
KC-10, complete replacement is still
under study by the Air Force. Despite increased maintenance costs,
studies conclude many of the aircraft could be flown until 2040,
with ages reaching 80 years before reaching lifetime flying hour
limits.
Development
The KC-135 is derived from the original
Boeing jet transport "proof of concept" demonstrator,
the
Boeing 367-80 (commonly called the
"Dash-80"). As such, it has a narrower
fuselage and is shorter than the
Boeing 707 jetliner. Boeing gave the tanker the
designation of Model 717. The 367-80 was the basic design for the
commercial Boeing 707 passenger aircraft as well as the KC-135A
Stratotanker.
In 1954 the
USAF's
Strategic Air Command ordered the
first 29 of its future fleet of 732.
The first aircraft
flew in August 1956 and the initial production Stratotanker was
delivered to Castle Air Force Base
, California
, in June 1957. The last KC-135 was delivered
to the Air Force in 1965.

USAF KC-135R boom operator view
Developed in the late 1950s, the basic airframe is characterized by
swept wings and
tail, four underwing
mounted engine pods, a
horizontal
stabilizer mounted on the fuselage near the bottom of the
vertical stabilizer with
positive
dihedral on the two
horizontal planes and a hi-frequency radio antenna which protrudes
forward from the top of the vertical fin or stabilizer. These basic
features make it strongly resemble the commercial Boeing 707 and
720 aircraft, although it is actually a different aircraft.
The
Strategic Air Command
(SAC) had the KC-135 Stratotanker in service with Regular Air Force
SAC units from 1957 through 1992 and with SAC-gained
Air National Guard (ANG) and
Air Force Reserve (AFRES) units from 1975
through 1992.
Following a major USAF reorganization that resulted in the
inactivation of SAC in 1992, most KC-135s were re-assigned to the
newly-created
Air Mobility
Command (AMC). While AMC gained the preponderance of the aerial
refueling mission, a small number of KC-135s were also assigned to
directly
United
States Air Forces in Europe (USAFE),
Pacific Air Forces (PACAF) and the
Air Education and
Training Command (AETC). All
Air Force Reserve Command (AFRC)
KC-135s and most of the
Air National
Guard (ANG) KC-135 fleet became operationally-gained by AMC,
while
Alaska Air National
Guard and
Hawaii Air
National Guard KC-135s became operationally-gained by
PACAF.
Reconnaissance and command post
variants of the aircraft, including the
RC-135 Rivet Joint and
EC-135 Looking Glass Post Attack Command
& Control Systems were operated by SAC from 1963 through 1992,
when they were re-assigned to the
Air
Combat Command (ACC). The USAF EC-135 Looking Glass was
subsequently replaced in its role by the
U.S. Navy E-6 Mercury aircraft, a new build airframe based
on the Boeing 707 and KC-135.
General upgrades
The KC-135Q was the variant modified to carry the
JP-7 fuel necessary for the
SR-71
Blackbird and air-refuelable versions of the
U-2, segregating the JP-7 from the KC-135's own
fuel supply (the body tanks carrying JP-7, and the wing tanks
carrying JP-4 or JP-8). When the KC-135Q model received the CFM-56
engines, it was redesignated the KC-135T model, which was capable
of separating the main body tanks from the wing tanks where the
KC-135 draws its engine fuel. The only external difference between
a KC-135R and a KC-135T is the presence of a clear window on the
underside of the empennage of the KC-135T where a remote controlled
searchlight is mounted. It also has two ground refueling ports,
located in each rear wheel well so ground crews can fuel both the
body tanks and wing tanks separately.
Eight KC-135R aircraft are receiver-capable tankers, commonly
referred to as KC-135R(RT).
All eight aircraft were with the 22d Air Refueling Wing at McConnell AFB
, KS as of 1994. They are primarily used for
force extension and Special Operations missions, and are crewed by
highly qualified receiver capable crews. If not used for the
receiver mission, these aircraft can be flown just like any other
KC-135R.
In order to expand the KC-135's capabilities and improve its
reliability, the aircraft has undergone a number of upgrades. Among
these was the Pacer-CRAG program
(CRAG=
Compass, R
adar
A
nd G
PS) which ran from 1999 to 2002
and modified all the aircraft in the inventory to eliminate the
Navigator position from the flight crew. The program
development was done by Rockwell
Collins in Iowa
and
installation was performed by BAE Systems
at the Mojave Airport
in California
.
The latest block upgrade to the KC-135 is
Block 40.3 which allows the KC-135 to comply with CNS/ATM.
Re-engining
All KC-135s were originally equipped with Pratt & Whitney
J-57-P-59W turbojet engines which produced 10,000 lbf of
thrust dry, and approximately 13,000 lbf of thrust wet. Wet
thrust is achieved through the use of water injection on takeoff.
670 gallons of water are injected into the engines over the course
of two and a half minutes. This water allows a second set of fuel
injectors to activate without melting the turbine buckets. The
water turns to steam and is ejected out the rear of the engine,
increasing the mass through the engine and increasing thrust. The
engine runs a little hotter, with more engine noise. In the 1980s
the first modification program re-engined 157
Air Force Reserve (AFRES) and
Air National Guard (ANG) tankers with the
Pratt & Whitney
TF-33-PW-102 engines from 707 airliners retired in the late
1970s and early 1980s. The re-engined tanker, designated the
KC-135E, was 14% more fuel efficient than the KC-135A and could
offload 20% more fuel on long duration flights. (The difference is
that the A-model weighed only 104,000 lb empty, while the
E-model weighed 115,000 lb empty. But the maximum takeoff
weight was not increased for the E-model. Therefore, the A-model
could takeoff with 200,000 lb of fuel, while the E-model could
only takeoff with 190,000 lb of fuel.) Only the KC-135E
aircraft were equipped with thrust-reversers for takeoff aborts and
shorter landing roll-outs. The KC-135E fleet has since either been
re-engined into the R-model configuration or placed into "XJ" or
long term storage, as Congress has prevented the Air Force from
formally retiring them. The final KC-135E, tail number 56-3630, was
delivered by the 101st Air Refueling Wing of the Maine ANG to the
309th Aerospace Maintenance and Regeneration Group (AMARG) at
Davis-Monthan AFB in September 2009.
The second modification program re-engined 500 aircraft with new
CFM International CFM56
(F-108 for the military designation) engines produced by General
Electric and Snecma. The CFM-56 turbofans are capable of producing
approximately 22,500 lbf of thrust, nearly a 100% increase in
power compared to the original J-57 engines. The re-engined tanker,
designated either the KC-135R or KC-135T, can offload up to 50%
more fuel (on a long duration sortie), is 25% more fuel efficient,
costs 25% less to operate and is 96% quieter than the KC-135A
(sideline noise levels at takeoff were reduced from 126 to 99
decibels).
The KC-135R's operational range is 60% greater than the KC-135E for
comparable fuel offloads, providing a wider range of basing
options.
No longer in consideration, upgrading the remaining KC-135E into
KC-135R would have cost about three billion dollars, about 24
million dollars per aircraft. According to Air Force data, the
KC-135 fleet had a total operation and support cost in fiscal year
2001 of about $2.2 billion. The older E model aircraft averaged
total costs of about $4.6 million per aircraft, while the R models
averaged about $3.7 million per aircraft. Those costs include
personnel, fuel, maintenance, modifications, and spare parts.
Multi-Point Refueling System program

Multi-Point Refueling System
paradrogue and hose.
The hose is 74 feet long when fully trailed.
This program adds refueling pods to the KC-135's wings. The pods
allow refueling of U.S. Navy, U.S. Marine Corps and most NATO
tactical jet aircraft while keeping the tail-mounted refueling
boom. The pods themselves are Flight Refueling Limited (FRL) MK32B
model pods. This allows the tanker to refuel two receivers at the
same time, which increases throughput compared to the boom drogue
adapter.
Research and development
Besides
its primary role as an inflight aircraft refueler, the KC-135,
designated NKC-135, has assisted in several research projects at
the NASA
Dryden Flight
Research Center
at Edwards Air Force Base
, California. One such project occurred between 1979 and
1980 when special wingtip "winglets",
developed by Richard Whitcomb of
the Langley
Research Center
, were tested at Dryden, using an NKC-135A tanker
loaned to NASA by the Air Force. Winglets are small, nearly
vertical fins installed on an aircraft's wing tips. The results of
the research showed that
drag was
reduced and
range could be
increased by as much as 7 percent at cruise speeds. Winglets are
now being incorporated into most new commercial and military
transport jets, as well as business aviation jets.
NASA also has operated several KC-135 aircraft (without the tanker
equipment installed) as their infamous
Vomit
Comet zero-gravity simulator aircraft. The longest-serving
(1973 to 1995) version was KC-135A, AF Ser. No. 59-1481, named
Weightless Wonder IV and registered as N930NA.
Electronic warfare
A number of KC-135A and KC-135B aircraft have been modified to
EC-135,
RC-135
and
OC-135 configurations for use in several
different roles.
Design

Flight deck of KC-135R; instrument
panel has been modified under the Pacer-CRAG program
The KC-135R has four
turbofan engines,
mounted under 35-degree swept wings, which power it to takeoffs at
gross weights up to 322,500 pounds (146,300 kg). Nearly all
internal fuel can be pumped through the tanker's
flying boom, the KC-135's primary fuel transfer
method. A special shuttlecock-shaped drogue, attached to and
trailing behind the flying boom, may be used to refuel aircraft
fitted with probes. A
boom
operator stationed in the rear of the aircraft controls the
boom while lying prone. A cargo deck above the refueling system can
hold a mixed load of passengers and cargo. Depending on fuel
storage configuration, the KC-135 can carry up to 83,000 pounds
(37,600 kg) of cargo.
Operational history

An F-15 backs out after refueling from
a KC-135R.
The KC-135 was initially purchased to support bombers of the
Strategic Air Command, but by the late 1960s, in the
Southeast Asia the KC-135 Stratotanker's ability
as a force multiplier came to the fore. Midair refueling of
F-105 and
F-4
fighter-bombers as well as B-52 bombers brought far-flung bombing
targets within reach, and allowed fighter missions to spend hours
at the front, rather than just a few minutes, due to their limited
fuel reserves. KC-135 crews refueled both Air Force and Navy /
Marine Corp aircraft, though they would have to change to
probe and drogue adapters depending upon
the mission. Crews also helped to bring in damaged aircraft which
could fly while being fed by fuel to a landing site. KC-135s
continued their tactical support role in later conflicts such as
Desert Storm and current aerial
strategy.
Air Mobility Command (AMC)
manages more than 481 Stratotankers, of which the
Air Force Reserve Command
(
AFRC) and
Air National Guard
(
ANG) fly 292 in support of AMC's mission as on
April 2008.
Replacing the KC-135
As of 2006, the KC-135E fleet was flying an annual average of 350
hours per aircraft and the KC-135R fleet is flying an annual
average of 710 hours per aircraft. The KC-135 fleet is currently
flying double its planned yearly flying hour program to meet
airborne refueling requirements, and has resulted in higher than
forecast usage and sustainment costs.

KC-135Rs at twilight on the
flightline
The Air Force projects that E and R models have lifetime flying
hour limits of 36,000 and 39,000 hours, respectively. According to
the Air Force, only a few KC-135s would reach these limits before
2040, but at that time some of the aircraft would be about 80 years
old. The Air Force estimates that their current fleet of KC-135s
have between 12,000 to 14,000 flying hours on them-only 33 percent
of the lifetime flying hour limit. Nevertheless these aircraft are
over 40 years old and maintenance costs are increasing, with
airframe corrosion being the worst problem.
Between 1993 and 2003, the amount of KC-135 depot maintenance work
doubled, and the overhaul cost per aircraft tripled. In 1996 it
cost $8,400 per flight hour for the KC-135, and in 2002 this had
grown to $11,000. The Air Force’s 15-year cost estimates project
further significant growth through fiscal year 2017. For example,
operations and support costs for the KC-135 fleet are estimated to
grow from about $2.2 billion in fiscal year 2003 to $5.1 billion
(2003 dollars) in fiscal year 2017, an increase of $2.9 billion, or
over 130 percent, which represents an annual growth rate of about
6.2 percent.
The USAF has decided to replace the KC-135 fleet. However, since
there are over 500 KC-135s, these aircraft will be replaced
gradually, with the first batch of about 100 aircraft to be
replaced in the current buy. The effort to replace the KC-135 has
been marked by intense controversy.
Initially the first batch of replacement planes was to be an air
tanker version of the
Boeing 767, leased
from
Boeing. In 2003, this was changed to
contract where the Air Force would purchase 80 KC-767 aircraft and
lease 20 more. In December 2003, the Pentagon froze the contract
and in January 2006, the
KC-767
contract was canceled. This followed public revelations of
corruption in how the contract was awarded, as well as controversy
regarding the original leasing rather than outright purchase
agreement. Then Secretary of Defense Rumsfeld stated that this move
will in no way impair the Air Force's ability to deliver the
mission of the KC-767, which will be accomplished by continuing
upgrades to the KC-135 and
KC-10
Extender fleet.
In January 2007, the U.S. Air Force formally launched the
KC-X program with a
request for proposal (RFP). KC-X is
first phase of three acquisition programs to replace the KC-135
fleet. On 29 February 2008, the US Defense Department announced
that it had selected the
EADS/
Northrop Grumman "KC-30" (to be designated the
KC-45A) over the Boeing KC-767. On 18
June 2008, the US
Government Accountability
Office sustained Boeing's protest of the selection of the
Northrop Grumman/EADS's tanker. The status of the KC-45A is in
doubt and the Air Force may have to rebid the contract, potentially
reversing their earlier decision.
In March 2009 the Air Force indicated that KC-135s would require
additional skin replacement (lower wing skins were replaced by a
newer alloy by Boeing in 1975-1988) to allow their continued use
beyond 2018.
Operators
Note
Italy
has been reported in some sources as operating
several KC-135s, however these are actually Boeing 707-300s
converted to tanker configuration.
Variants

Active KC 135
- KC-135A
- Original production version powered by four Pratt & Whitney J57, 732
built.
- NKC-135A
- Test-configured KC-135A
- KC-135B
- Airborne command post version with 17 built equipped with
turbofan engines. Provided with in-flight refueling capability and
redesignated EC-135C.
- KC-135D
- All four RC-135As were modified to partial KC-135A
configuration in 1979. They were given a unique designation as they
differed from the KC-135A in that they were built with a flight
engineers position on the flight deck. The flight engineer's
position was removed when the aircraft were modified to KC-135
standards but they retained their electrically-powered wing flap
secondary (emergency) drive mechanism and second air conditioning
pack which had been used to cool the RC-135As on-board
photo-mapping systems. Later re-engined with Pratt & Whitney TF33 engines
and a cockpit update to KC-135E standards in 1990.
- KC-135E
- Air National Guard and Air Force Reserve KC-135As re-engined
with Pratt & Whitney
TF-33-PW-102 engines from retired 707 airliners (161 modified).
These
aircraft are being retired to Davis-Monthan Air Force Base
and replaced with R models.
- NKC-135E
- Test-configured KC-135E
- KC-135Q
- KC-135As modified to carry JP-7 fuel
necessary for the SR-71 Blackbird, 56
modified, survivors to KC-135T.
- KC-135(K)R
- KC-135As re-engined with CFM-56
engines.
- KC-135R(RT)
- Receiver-capable KC-135R Stratotanker, 8 modified with either a
Boeing or LTV receiver system and a secure voice SATCOM radio.
- KC-135T
- KC-135Q re-engined with CFM-56 engines, 54 modified.
- EC-135Y
- An airborne command post modified in 1984 to support CINCCENT.
Aircraft 55-3125 was the only EC-135Y. Unlike its sister EC-135N,
it was a true tanker that could also receive in-flight refueling.
Pratt & Whitney
TF-33-PW-102. Currently retired at AMARC.
See
C-135 Stratolifter, and
related articles for other C-135 family variants.
Specifications (KC-135R)
See also

Six KC-135 Stratotankers demonstrate
the elephant walk formation.
References
- "Historical Perspective, Start of a PROUD
MISSION", Boeing Frontiers, July 2006.
- Hopkins, pp. 71-72.
-
http://www.janes.com/articles/Janes-Aircraft-Upgrades/Boeing-KC-135--Rockwell-Collins-Pacer-CRAG-Avionics-Upgrade-United-States.html
- "BAE SYSTEMS delivers final Pacer CRAG KC-135", Aerotech
News and Review, 2002-09-20
- Beckham, Staff Sgt. Tim. "Final KC-135E retires at Davis-Monthan". AF news, 25
September 2009.
- http://boeing.com/defense-space/military/kc135/index.html
- KC-135E, Globalsecurity.org
- http://www.gao.gov/new.items/d03938t.pdf
-
http://www.globalsecurity.org/military/systems/aircraft/kc-135r-mprsp.htm
- KC-135 Aircraft Photo Gallery Contact
Sheet
- C-135 Variants - Part 2, by Jennings
Heilig
- C-135 Variants, Part 6 by Jennings
Heilig
- http://www.boeing.com/commercial/707family/index.html
- KC-135 fact sheet, USAF, September 2008.
-
http://www.globalsecurity.org/military/library/congress/2006_hr/060228-bartlett.pdf
- KC-135E. globalsecurity.org
- When Aircraft Get Old. Air Force magazine
- GAO-04-349, MILITARY AIRCRAFT: DOD Needs to
Determine Its Aerial Refueling Aircraft Requirements
- Tanker Twilight Zone, Air Force magazine,
February 2004, Vol. 87, No. 2.
- "Air Force Posts Request for Proposals for
Tankers", US DoD, 30 January 2007.
- "Tanker contract award announced", US Air Force, 29
February 2008.
- Thin Skin, Aviation Week & Space
Technology, 70, 10 (9 March 2000), p. 18
-
http://www.boeing.com/news/releases/1999/news_release_990910n.htm
- Mehuron, Tamar A., Assoc. Editor. 2008 USAF Almanac, Fact and Figures, Air Force
Magazine, May 2008.
- "Boeing wins Italian bid military 767s", Italy
operates 4 KC-135s, SeattlePi.com, 2001-07-10
- Aeroflight's listing of Italian Air Force
aircraft
- Airframe
tracking information from Airlinerlist.com
- Donald, David. "Boeing Model 717 (C/KC-135
Stratoliner/Stratotanker." The Complete Encyclopedia of World
Aircraft. Barnes & Nobel Books, 1997. ISBN
0-7607-0592-5.
- DoD 4120.14L, Model Designation of Military Aerospace
Vehicles, 12 May 2004
- Hopkins, p.144
- Pither, Page 73
- Hopkins, pp. 142-144.
- Pither, p. 73.
- Baker, MSgt Burke. "48-year-old KC-135 retires", Air Force news, 22 May
2008.
- Tony Pither, The Boeing 707 720 and C-135, Air-Britain
(Historians) Ltd, England, 1998, ISBN 0 85130 236 X.
External links