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The Gripen Fourth Generation Fighter
The
Gripen fighter aircraft is designed and built by Saab of Sweden and
marketed by Gripen International, a joint venture by Saab and BAE
Systems.
History
The first Gripen prototype flew in December 1988. This was
the original A and B version, which was designed as an air defence
fighter. The development of the C and D version, now also known as the
EBS or export baseline version, started in the late 1990s, and by 2003
was flying with most of the functionalities intact. This development was
a major upgrade of the Gripen A and B to produce a 4th generation
multi-role fighter aircraft. The SAAF version is based on the EBS
version with a few unique requirements embedded. The first aircraft
destined for the SAAF was unveiled at Saab on 28 October 2005 and first
flew on 11 November 2005.
General Description
The Gripen is described as a 4th generation swing-role fighter aircraft.
Aerodynamically it utilises an inherently unstable design, coupled with
fly-by-wire control, a canard-delta wing layout and a good power to
weight ratio to provide a very agile aircraft capable of sustaining 9
“g”. Its fully integrated, digital avionics design allows for seamless
integration of systems and data fusion, providing the aircrew with a
superior awareness level and extremely benign flying characteristics.
Aircrew awareness is further enhanced by the data link capability,
linking air platforms and/or air platforms and ground stations. Very
good survivability is ensured by a combination of small size, inherent
stealth design characteristics, high agility and a state of the art
active and passive electronic warfare system. The combination of the
above factors ensures very high operational effectivity.
The Gripen system includes a state of the art, fully
encompassing training system, centred on a Computer Based Training
System (CBTS) and two Squadron Level Mission Trainers. Flying training
is further enhanced by the availability of the dual seat aircraft. The
systems are utilised by air and ground crews and are designed to cater
for all levels of training, from initial conversion training to advanced
operational/technical training.
Application and Placement
The Gripen C (single seat) and D (dual seat) fighter aircraft will
replace the Cheetah C and D aircraft as the SAAF's fighter capability.
They will be based at AFB Makhado in the facilities currently utilised
by 2 Squadron. The unit will retain its number, ie 2 Squadron.
The Gripen C and D aircraft will be utilised in the following roles:
a. Air Defence
b. Surface Attack
c. Reconnaissance
d. Operational Conversion Training
Programme Status
The first Gripen, the flight test instrumented aircraft, arrived in
South Africa on 17 July 2006. This aircraft will be utilised to conduct
a Development Test and Evaluation (DT&E) phase under the auspices of
Saab. This phase will be conducted at the Test Flight and Development
Centre (TFDC) at AFB Overberg, also utilising the Denel Overberg Test
Range (OTR). This aircraft will be handed over to the SAAF during the
1st quarter of 2008. Training of ground crew will commence in 2007.
Deliveries of aircraft and training and logistic systems will commence
during 2008, with flying training planned to commence in the 4th quarter
of 2008. Deliveries of aircraft will be completed by the end of 2011,
with full system handover to the SAAF at the beginning of 2012. The
Gripen system is designed for a service life of at least thirty years

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Performance
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Gripen Fighter |
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Crew: |
1-2 |
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Length: |
14.1 m (46 ft 3 in) |
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Wingspan: |
8.4 m (27 ft 7 in)
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Height: |
4.5 m (14 ft 9 in)
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Wing area: |
25.54 m2 (274.9 ft2)
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Empty weight:
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6,620 kg (14,600
lb) |
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Loaded weight:
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8,720 kg (19,200 lb)
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Max takeoff weight:
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14,000 kg (31,000 lb)-
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Powerplant: |
1× Volvo Aero RM12
(GE404) afterburning turbofan, 54 kN
dry, 80 kN with afterburner (12,000 lbf
/ 18,100 lbf) |
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Wheel track: |
2.4 m (7 ft 10 in) |
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Maximum speed:
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Mach 1,8 |
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Range: |
1200km (650Nm) (500 mi) |
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Service ceiling:
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15,000 m (50,000 ft) |
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Armament: |
1 x 27mm Mauser BK-27
cannon (C version only)
Provision for up to 6 x short-range
infrared A-A missiles
Provision for up to 4 x medium-range
electro-magnetic A-A missiles
Provision for Mk81/Mk82 free-fall bombs
and laser-guided bombs
The Gripen is also cleared for various
air-to-surface missile |
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Major enhancements
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A full
multi-role capability, ie air-to-air,
air-to-ground and reconnaissance modes.
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Full
Authority Digital Engine Control (FADEC).
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Air
refuelling capability.
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On-board
Oxygen Generation System (OBOGS).
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Upgrading of
all major computers.
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Upgraded
avionics architecture.
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Full colour
displays.
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Suitability for the African Scenario
Based on the Swedish doctrine of
deployed operations from road bases, the Gripen is ideally suited to
the African environment. Its take-off and landing distances are very
modest and together with the Auxiliary Power Unit (APU), it supports
short duration deployed operations, with very little ground-support
equipment, from austere locations. The on-board Built-in Test
Equipment reduces fault-finding time and, together with simple
swapping of Line Replaceable Units (LRUs), the turn-around time is
significantly reduced and the process simplified. The environmental
control system (ECS) has also been adapted to cope with the cooling
demands of the African scenario.
The communications and identification systems have been designed
according to the SANDF Combat Net Interoperability Standards.
Therefore, the aircraft avionics can interact with the SANDF Command
and Control systems through the data link system, supporting the
netcentric warfare concept. Regarding armament, the full range of
locally produced missiles and bombs will be cleared for use on
Gripen.
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