The Hawk Lead In Fighter Trainer
The
South African Air Force (SAAF) Hawk Mark 120 Lead In Fighter Trainer
(LIFT) aircraft is a derivative of the BAE SYSTEMS Mark 100 Hawk series,
designed and built by BAE SYSTEMS of the United Kingdom since the
mid-1990s. The engine, powering the Hawk LIFT is a Rolls Royce/Turbomeca
Adour Mark 951 engine, which is a newly developed upgrade from the Adour
871, with South Africa as the launch customer. The aircraft has a newly
developed local Avionics Suite by Advanced Technlogies Engineering
(ATE). Local Industry has been involved in various elements of the
Engineering, Training and Support deliverables.
History
The first two-seater Hawk T Mk 1 series was designed and delivered to
the Royal Air Force in the mid-seventies. This evolved into the Hawk Mk
50/60 series through to the nineties, when a major 7 station wing
modernisation and nose cone was done on the Mk 100 series. The first
single-seater Hawk 200 trainer/light fighter was delivered to the Royal
Oman Air Force in the early nineties. A naval version of the two-seater
named Goshawk, was designed for the United States Navy in 1991. To date
around 750 Hawk aircraft are being operated in more than 16 countries
worldwide, flying in excess of 1,4 million flying hours. The NATO Flight
Training Centre (NFTC) in Canada trains fighter pilots from a number of
additional countries, and this makes the Hawk unique. By means of a
well-established Hawk User Group for Aircrew and Groundcrew, an
excellent exchange of knowledge and networking has been established.
South Africa has participated therein since 2000 and will host the next
User Group in 2007. Since South Africa signed up for the Hawk 100
series, the Indian Air Force, Royal Air Force and the Bahrain Air Force
acquired versions of this aircraft. This bodes well for the future
sustainability of Hawk worldwide.
General Description
The Hawk is a transonic lead-in fighter trainer (LIFT) encompassing
ideal handling characteristics for fighter training and is capable of
demonstrating supersonic flight in a dive. The aircraft can train
aspirant fighter pilots in all aspects of modern fighter flying. In the
case of the Hawk Mk 120, the cockpit has been specifically tailored to
seamlessly and cost effectively train pilots graduating from the SAAF
Astra basic trainer to the SAAF Gripen front line fighter.
The Adour 951 engine introduces full authority digital engine control (FADEC),
care free handling and a maximum thrust output of 6 500 lbs. The power
to weight ratio and good sustained turn rates provide an ideal flight
envelope and performance domain to step from the Astra to the Gripen.
The Hawk has an open architecture avionics system which allows for
efficient training in a systems environment and gives the aircrew a high
situational awareness. Aircrew awareness is further enhanced by a
simulated radar, multi-functional displays and hands-on throttle and
stick (HOTAS). External fuel tanks and an air refuelling capability
enhance the range of the aircraft. The combination of the above factors
ensures a very capable lead-in fighter-trainer aircraft.
Application and Placement
The primary role of the Hawk Mk 120 is all aspects of Air Combat
Training for the SAAF's air and ground crews from aircraft type
conversion to full mission training during a deployment. This will
include Joint Training with the other Arms of Service and participation
in Operational training exercises. The 24 Hawks replace the 250 Impala
Mk 1 and Mk 2 aircraft phased out in late 2005. They will be based at
AFB Makhado and the Unit will retain its name of 85 Combat Flying
School. The unit relocated from AFB Hoedspruit to AFB Makhado in January
2005.
By nature of the Hawk's inherent training capabilities, certain
collateral operational tasks in a low threat environment are envisaged
for the aircraft. These will be developed and implemented over the next
few years and may include the following:
a. Search and Rescue
b. Communications
c. Border Patrol
d. Reconnaissance
e. Limited Close Air Support.
Programme Status
The Hawk Project has entered the Implementation Phase and ten aircraft
have been delivered to date. The initial cadre of instructor and unit
personnel training is well underway, most of the necessary facilities
are in place and the first Hawk learner Aircrew course is due to
commence in a year. The required Engineering, Training and Logistics
support are being implemented. These will continue to be delivered,
along with the remaining 14 aircraft and the full system will be handed
over to the SAAF in 2008, at which point steady-state operations will
have been achieved. Thereafter the Hawk LIFT System is expected to be in
service with the SAAF for at least 30 years, in all likelihood closer to
40 years.

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Performance
| |

Hawk Lead in Fighter
Trainer |
|
Crew: |
1-2 |
|
Length: |
12.43 m (40.78 ft) |
|
Wingspan: |
9.075 m (29.77 ft)
|
|
Height: |
3.98 m (13.06 ft)
|
|
Empty weight:
|
4,530 kg (9,987
lb) |
|
Loaded weight:
|
8,720 kg (19,200 lb)
|
|
Max takeoff weight:
|
9,100 kg (20,062 lb)
|
|
Powerplant: |
1× Adour Mk 951 with 6500
lb thrust |
|
Wheel track: |
3.47 m (11.38 ft) |
|
Maximum speed:
|
500+ kts (1 000 km/h) |
|
Range: |
Around 900 Nm clean. Can carry drop tanks and do A-A refueling for extended ranges |
|
Service ceiling:
|
40,000
ft plus |
|
Armament: |
5 x underwing and 2 x wingtip stations
1 x 30mm Aden gun pod
Provision for up to 2 x wingtip
short-range infrared A-A missiles
5 x CBLS2000 with 4 x 12.5 kg smoke
and flash practice bombs
Series of local Mk 81 bombs
Simulated weapons (all of the above) |
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Suitability for the Local Scenario
The Hawk 100 series airframe was
designed to be operated around the world and has proven itself
worthy in this regard. The upgraded thrust of the engine of the SAAF
Hawk will largely overcome previous limitations of operating in very
hot and high altitude conditions. A large part of the Avionics
Suite, Training System and Logistics Support equipment is locally
developed and/or manufactured. Much effort has been placed on the
Integrated Logistics and Life Cycle Cost Management processes to
maximise local capabilities and reduce life cycle costs to the SAAF.
The take-off and landing distances of the Hawk are well within the
available capabilities and, together with the Auxiliary Power Unit (APU),
can be easily deployed away from the Main Operating Base. The
environmental control system (ECS) has also been improved to cope
with the cooling demands of the African scenario. Lastly, all the
current weapons on Hawk are of local manufacture.
The communications and identification systems have been designed
according to the SANDF Combat Net Interoperability Standards.
Therefore, the aircraft avionics can adequately interact with the
SANDF Command and Control systems to achieve meaningful training in
this regard.
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