|
F-35
Lightning II
The F-35 is a major transatlantic
project involving the US and its European
allies. The project started life in
the mid-1990s as the Anglo-American
Joint Strike Fighter (JSF) -- also
called the Joint Combat Aircraft (JCA)
by the UK -- developed by Lockheed
Martin, Northrop Grumman and BAE Systems
to replace the USAF’s F-16 Fighting
Falcon and A-10 Thunderbolt II, the
US Navy’s F/A-18 Hornet, the USMC’s
F/A-18 Hornet and AV-8 Harrier II,
and Britain’s Harrier GR9 fleet jointly
operated by the RAF and the Royal
Navy's Fleet Air Arm. The project
has since been joined by Australia,
Canada, Denmark, Italy, the Netherlands,
Norway and Turkey who signed a memorandum
of understanding (MoU) to join the
System Development and Demonstration
(SDD) phase of the project in 2001.
Israel and Singapore signed-up for
Security Co-operative Participation
(SCP) in 2003. The F-35 Lightning
II will replace the F/A-18 Hornet
and/or F-16 Fighting Falcon fighters
operated by these countries. Singapore
recently acquired 24 F-15SG Strike
Eagles as an interim fighter to replace
the F-5 Tiger II and A-4 Skyhawk until
the F-35 becomes available with deliveries
due in 2008-2010. It is, however,
likely that this aircraft will continue
to operate alongside the F-35 once
it enters service.
The F-35 Lightning
II is a single-seat fighter with stealth
capabilities in conventional take-off
and landing (CTOL), carrier-based
variant (CV) and short take-off and
vertical landing (STOVL) configurations.
The aircraft will be powered by a
single turbofan providing a maximum
speed of Mach 1.8 and will be capable
of carrying up to 15,000 lb of ordnance.
Two different versions of the aircraft’s
power plant are being developed by
GE Aviation, Pratt & Whitney and Rolls-Royce.
The CTOL (F-35A) version and slightly
larger CV (F-35C) variant will be
powered by a single Pratt & Whitney
F135 turbofan or the F136 being developed
by the GE Rolls-Royce Fighter Engine
Team (FET). The STOVL variant (F-35B)
will be powered either by a F135 or
F136 featuring a Rolls-Royce-designed
two-stage lift fan and three-bearing
swivelling nozzles to provide vertical
and forward thrust. Pratt & Whitney's
F135 will be used to power F-35B test
models until 2010. The company was
awarded its first F135 production
contract worth US$69.3 million (EUR47.3
million) in September 2007 to cover
the delivery of engines for two F-35A
models in 2009.
The US is the main
financial contributor to the programme
with US$5.3 billion (EUR3.6 billion)
allocated in 2007. Some US$6.2 billion
(EUR4.2 billion) has been allocated
in 2008, which will include the procurement
of 12 aircraft for testing purposes.
The other nations involved in the
project are designated partners at
three levels (I, II, III). Each level
provides different industrial participation
and how many staff are assigned to
the F-35's programme office in the
US. Level I and II partners have some
influence in the F-35's design and
development to meet their own specific
national requirements. The UK is a
Level I partner and is contributing
some US$2.0 billion (EUR1.4 billion),
about ten per cent of the cost of
the SDD phase. As Level I partner,
the UK has the biggest industrial
participation after the US and should
also financially gain more from sales.
Italy and the Netherlands are Level
II partners and are contributing US$1.8
billion (EUR1.2 billion), while Australia,
Canada, Denmark, Norway and Turkey
are Level III partners and are together
contributing some US$725 million (EUR494
million) to the overall programme.
Israel and Singapore are reportedly
each paying less than US$50 million
(EUR34 million) through their SCP
agreements with their aircraft likely
to be purchased through the US's Foreign
Military Sales (FMS) scheme.
Most of the project
partners will acquire the F-35A with
the UK and the USMC due to purchase
the
F-35B and the US Navy the F-35C. The
USAF was looking at purchasing a small
number of F-35B variants, but the
recent US$300 million (EUR206 million)
upgrade to some of its A-10 Thunderbolt
II should keep that aircraft in service
until 2020. Italy's planned procurement
of about 131 F-35s should include
22 F-35Bs to replace the Italian Navy's
AV-8B Harrier II+. Denmark and Norway
are still considering modified versions
of Sweden's JAS-39 Gripen as an alternative
to the F-35A with a decision due in
2009.
Project
partners
The first flight
of the F-35 Lightning II (AA-1) took
place at Lockheed Martin’s site in
Fort Worth, Texas in the US on 15
December 2006. The F-35B prototype
(BF-1) is scheduled to make its maiden
flight in May 2008. The F-35B will
initially be powered by the F135 engine,
but will feature the F136 in later
test flights after 2010. Initial deliveries
for the US Marine Corps for training
purposes are expected in 2011. The
F-35C is expected to make its first
flight in 2009. The SDD phase will
see the construction of 19 aircraft,
comprising 13 for flight testing and
six for ground testing. Other than
the US, some partners will make initial
purchases of production F-35s fitted
with test instrumentation for the
Initial Operational Test & Evaluation
(IOT&E) during the programme's overall
Verification and Test (V&T) stage
in the run-up to full deliveries.
Orders for these models are expected
to begin in 2008. The Netherlands
confirmed in October 2007 that it
plans to order its first IOT&E
F-35A at a cost of US$124 million
(EUR86 million) by 2009, with a second
to be ordered in 2010. The UK plans
to purchase up two F-35s for the OT&E
stage. Unit cost of the production
F-35 is expected to be lower than
the OT&E cost. The current unit
cost as detailed in the US DoD’s FY2009
budget request is US$225 million (EUR155
million). A 2006 estimate put the
unit cost by 2014 when the aircraft
is at its full production rate at
US$48 million (EUR33 million) for
the F-35A, US$62 million (EUR42 million)
for the F-35B and US$63 million (EUR43
million) for the F-35C.
All countries have
recently joined the next phase of
the project, the Production, Sustainment
and Follow-on Development (PSFD).
Production of most of the aircraft
will take place in the US with Lockheed
Martin the prime contractor building
the forward fuselage and wings at
Fort Worth, and Northrop Grumman at
Palmdale and El Segundo in California
the centre fuselage, weapons bay and
the aircraft’s AN/APG-81 Active Electronically
Scanned Array (AESA) radar. Northrop
Grumman is additionally working with
Lockheed Martin Missiles and Fire
Control on the F-35’s AN/AAQ-37
electro-optical distributed aperture
system (DAS). BAE Systems will build
the rear fuselage, tails and the F-35C’s
wing-folding mechanism at its Samlesbury
facility in the UK. It is additionally
responsible for providing the F-35's
nose-mounted Electro-Optical Targeting
System (EOTS), some of the avionics
and Electronic Warfare (EW) systems.
Other project partners will supply
components. Italy’s Alenia may undertake
the final assembly of all F-35s to
be delivered to European operators
with the exception of the UK, which
will assemble its own aircraft. Vision
Systems International (VSI), owned
by the US’s Rockwell Collins and EFW
Inc (a subsidiary of Israel’s Elbit
Systems), is developing the pilot’s
Helmet Mounted Display System (HMDS).
Deliveries are expected
to begin after 2012/13 with Initial
Operational Capability (IOC) shortly
afterwards. The project partners plan
to make an initial total purchase
of 2,400 F-35s at a cost of US$200
billion (EUR136 billion) with the
US planning to purchase up to 1,763
F-35A variants for the USAF and 680
F-35B/C variants for the US Navy and
USMC. Other possible European customers
include Greece, which requires up
to 40 aircraft to supplement its F-16
Fighting Falcon and Mirage 2000 fleet
and to ensure some degree of military
parity with Turkey. The F-35 would
be the ideal platform to replace the
EF-18A Hornet operated by the Spanish
Air Force. The F-35B would also be
a suitable replacement for the AV-8B
Harrier II+ operated by the Spanish
Navy, while Belgium and Portugal could
order the F-35A in the future to replace
their F-16 Fighting Falcon fleets.
Data
Specifications
(F-35A)
Overall length: 15.37 m
Wing span: 10.65 m
Wing area: 42.7 m²
Overall height: 5.28 m
Weights
Max take-off weight: 60,000
lb (27,200 kg)
Max payload: 15,000 lb (6,800
kg)
Performance
Powerplant: F-35A/C: 1 x Pratt
& Whitney F135 or 1 x GE Rolls-Royce
FET F136 turbofan rated at 25,000
lbf (111 kN) dry and 40,000 lb (178
kN) with reheat.
F-35B: 1 x Pratt & Whitney F135 or
1 × GE Rolls-Royce FET F136 turbofan
rated at 40,000 lbf (178 kN) with
reheat when combined with 1 x Rolls-Royce
18,000 lbf (80 kN) lift fan.
Max speed: Mach 1.6+
Range: 2,200 km (F-35A)
Climb rate: classified
Max operating altitude: 19,812
m (65,000 ft)
General data
Crew: 1
G-limits: +9g to -3g (F-35A)
Armament: 1 x internal GAU-12/U
25 mm cannon (F-35A) or 1 x external
GAU-12/U 25 mm cannon pod (F-35B/C),
six external and four internal hardpoints
located in two weapons bays to carry
a variety of weapons and/or drop tanks,
including air-to-air missiles (AIM-9
Sidewinder, AIM-120 AMRAAM, AIM-132
ASRAAM) and air-to-ground ordnance
(GBU-10/12/16/24 Paveway II, III,
Brimstone, Storm Shadow, JDAM).
Radar: Northrop Grumman AN/APG-81
AESA
First flight: December 2006
(F-35A)
Status: undergoing development.
F-35
Lightning II main workshare
| It
is estimated that more than 120
companies are involved in the
F-35 programme. Other than the
companies listed below, Danish
defence companies have established
the Danish JSF Team (JSFDK) to
bid and co-operate for industrial
contracts. JSFDK comprises Falck
Schmidt Defence Systems AS (armoured
vehicle composites, masts, support),
IFAD AS (simulators), Systematic
AS (software) and Terma AS (aerostructures
and components). The Australian
government and about 21 major
Australian firms have formed the
"JSF Industry Team" for industrial
opportunities, while Norwegian
firms have formed the JSF International
Information Interchange Initiative
(JSF4I) to investigate common
maintenance and support of the
aircraft once in Norwegian service.
JSF4I includes Kongsberg Defence
and Aerospace, the consultancy
DNV (Det Norske Veritas), Corena
(maintenance software) and Jotne
EPM Technology (data management). |
|
| |
|
|
|
|
|
| forward
fuselage, wings, final assembly |
|
|
|
centre
fuselage, weapons bay, AN/APG-81
AESA radar,
AN/AAQ-37 electro-optical
distributed aperture system
(DAS) (with Lockheed Martin) |
|
|
|
| rear
fuselage, tails, wing-folding
mechanism (F-35C), EOTS,
ECW suite, radar warning
receiver, Full Authority
Digital Electronic Control
(FADEC) system |
|
|
|
|
|
|
|
|
|
| liftfan
(F-35B), three-bearing swivel
module, roll post ducts,
F136 engine (40% industrial
share) |
|
|
|
|
|
| upper
wing-box skins, lower wing-box
skins and nacelle skins |
|
|
|
| communications,
Navigation and Identification
(CNI) integrated body antenna |
|
Crane
Aerospace &
Electronics (US) |
|
|
|
|
| hydraulic
and wing fluid distribution
system, liftfan lubrication
system |
|
|
|
| electrical
power subsystem |
|
|
|
| electronic
control systems, electrical
power system, canopy frame |
|
GD
Armament and
Technical Products
(US) |
|
|
|
|
| weapons
bay door drive systems,
liftfan components, anti-icing
systems, landing gear, skin
panels |
|
Goodyear
Tire & Rubber
Company (US) |
|
|
|
|
| leading
edge flap actuators, F135/F136
gearbox |
|
|
|
|
|
|
| avionics,
fibre-optics and CNI high-speed
links |
|
|
|
|
|
|
| internal
navigation system, landing
gear wheels and brakes |
|
|
|
| internal
weapons bay, pneumatic weapon
delivery system, composite
structures, landing aid
antennas |
|
|
|
|
|
|
|
LM
Aero and
Progressive (US) |
|
| wingbox
parts, inner wing bulkheads,
F-35C wing structure components
|
|
|
|
primary
flight controls, leading-edge
flap drive systems,
wing-fold system |
|
|
|
| fuel
system, liftfan hydraulics,
F135/F136 controls |
|
|
|
|
|
|
|
|
|
|
Vision
Systems
International
(US) |
|
| Helmet
Mounted Display System (HMDS) |
|
Vought
Aircraft
Industries (US) |
|
|
|
|
|
|
|
| fuselage
and engine components, canopy |
|
Helmet
Integrated
Systems Ltd (UK) |
|
|
|
|
|
|
|
|
|
|
| High
Pressure Pure Air Generator
(HiPPAG), pneumatic weapons
ejection system |
|
|
|
| design
and second source supplier
of the wing box |
|
|
|
|
|
| |