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British Aerospace Hawk 100 &
200 (1 pics)
Hawk 100 at Le Bourget 2003
Hawk 100 at Le Bourget 2003
British
Aerospace Hawk 100
British
Aerospace Hawk 100 is an advanced two-seat weapons systems trainer with enhanced
ground attack capability. The aircraft provides fighter lead-in training and
navigator and weapons systems operator training. The nose of the Hawk 100 is
re-profiled to accommodate additional sensors and avionics systems, including a
forward-looking infrared (FLIR). The aircraft has seven hardpoints on the wings
for weapon payloads. Short-range air-to-air missiles can be mounted on the
wingtip missile launchers.
The Hawk
LIFT (Lead-In Fighter Trainer) derived from the Australian Hawk 127, is intended
to provide training for new-generation combat aircraft such as the Eurofighter
Typhoon or Saab Gripen, and features substantially improved cockpit and
avionics.
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Developing nation: |
United
Kingdom. |
|
Designer: |
Hawker
Siddeley. |
|
Manufacturer: |
BAE
Systems. |
|
Production
line: |
Brough,
East Yorkshire, UK. |
|
Task: |
Lead-in
fighter trainer. |
|
First flight: |
October 1, 1987, ZJ100. |
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First delivery: |
1993 to
Abu Dhabi. |
| |
British Aerospace Hawk
100 |
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Crew: |
2.
|
|
Ejection seat: |
Martin
Baker Mk.10 LH zero-zero. |
|
Wing
Span: |
-
9,39 m.
- 9,94 m with
tip-mounted AIM-9 Sidewinder. |
|
Wing
Area: |
16,69 m˛. |
|
Length fuselage: |
11,68 m. |
|
Length fuselage including probe: |
12,42 m. |
|
Height: |
3,99 m. |
|
Tail plane span: |
4,39 m. |
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Wheelbase: |
3,47 m. |
|
Wheel track: |
4,50 m. |
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Engines: |
One Rolls
Royce/Turboméca Adour Mk.871 rated 26.00 kN. |
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Weight: |
-
Empty: 4.400 Kg.
- Internal fuel: 1.304
kg.
- External fuel: 2 x
864 liter drop tanks.
- Max. payload: 3.084
Kg. |
|
Max.
take off weight: |
9.100 Kg. |
|
Max. speed: |
1.038 km/h
at 10.995 m. |
|
Service ceiling: |
13.545 m. |
|
Range: |
-
range 2.428 km without drop tanks.
-
ferry range 2.594 km with 864 liter drop tanks.
- combat radius 1.223
km with two 454 kg bombs or 510 km with seven BL755 cluster bombs or 259
km on a CAP with one 30 mm cannon and two AIM-9 Sidewinders for 3 hours
and 30 minutes. |
|
Performance: |
-
max. rate of climb at sea level 3.579 m per minute.
-
climb to 9.145 m in 7 minutes, 30 seconds.
- take-off run 640 m at
max. take-off weight.
- landing run 605 m at
max. landing weight. |
|
g limits: |
-4/+8 |
|
Radar: |
Northrop-Grumman AN/APG-66H pulse-Doppler X-band multimode radar. |
|
Centerline
hardpoints: |
1. |
|
Underwing
hardpoints: |
4. |
|
Wingtip
hardpoints: |
2. |
|
Weapons: |
- Aden 30 mm cannon
with 120 rounds.
- AIM-9L Sidewinder.
- 9 x 240 kg bombs.
- 9 x 113 kg bombs.
- 5 x 540 kg bombs.
- cluster bombs.
- Paveway II Bombs.
-
SNEB rocket pods. |
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Extra: |
Reconnaissance pod. |
British
Aerospace Hawk 200
The British Aerospace Hawk 200 is a
single-seat, lightweight multi-role combat aircraft for air defense and ground
attack missions. The first Hawk 200 demonstrator actually flew in May 19, 1986,
well before the Hawk 100 demonstrator, but was lost two months later in an
accident that killed test pilot Jim Hawkins, who either became disoriented or
ironically blacked out while demonstrating the aircraft's agility.
The Hawk 200 has the Adour 871 engine, combat
wing, and some of the other combat kit of the Hawk 100, but along with the
single seat configuration, which resulted in an entirely new fuselage from the
cockpit forward, also features a still taller tailfin; an optional fixed
in-flight refueling probe; and the Northrop-Grumman AN/APG-66H pulse-Doppler
X-band multimode radar, with ten air-to-air and ten air-to-surface modes.
The Hawk 200 has eleven external store points
with four underwing pylons, an under-fuselage pylon, and wingtip air-to-air
missile stations. The range of external stores includes air-to-air missiles, a
gunpod, rocket launchers, reconnaissance pod, retarded and free-fall bombs up to
540 kg, runway cratering, anti-personnel and light Armor bombs, cluster bombs,
practice bomb and rocket carriers and external fuel tanks.
|
Developing nation: |
United
Kingdom. |
|
Designer: |
British
Aerospace. |
|
Manufacturer: |
BAE
Systems. |
|
Production
line: |
Brough,
East Yorkshire, UK. |
|
Task: |
multi-role light
fighter. |
|
First flight: |
May 19, 1986, ZG200. |
| |
British Aerospace Hawk
200 |
|
Crew: |
1.
|
|
Ejection seat: |
Martin
Baker Mk.10 LH. |
|
Wing
Span: |
-
9,39 m.
- 9,94 m with
tip-mounted AIM-9 Sidewinder. |
|
Wing
Area: |
16,69 m˛. |
|
Length fuselage: |
11,33 m. |
|
Length fuselage including probe: |
12,07 m. |
|
Height: |
4,16 m. |
|
Tail plane span: |
4,39 m. |
|
Wheelbase: |
3,56 m. |
|
Wheel track: |
3,47 m. |
|
Engines: |
One Rolls
Royce/Turboméca Adour Mk.871 turbofan rated 26.00 kN. |
|
Weight: |
-
Empty: 4.450 Kg.
- Internal fuel: 1.361
kg.
- External fuel: 2 x
591 liter drop tanks.
- max. ordnance 3.493
kg. |
|
Max.
take off weight: |
9.100 Kg. |
|
Max. speed: |
1.019 km/h
at 2.440 m. |
|
Service ceiling: |
13.715 m. |
|
Range: |
-
range 2.428 km without drop tanks.
-
ferry range 3.610 km with 3x 864 liter drop tanks.
- combat radius 1.234
km with one Sea Eagle missile and two drop tanks or 945 km on a lo-lo-lo
reconnaissance mission with one reconnaissance pod and two drop tanks. |
|
Performance: |
-
max. rate of climb at sea level 3.508 m per minute.
- take-off run to 15 m
at max. take-off weight 2.134 m.
- landing run from 15 m
at max. landing weight 854 m with brake chute.
- landing run from 15 m
at max. landing weight 1.250 m without brake chute. |
|
g limits: |
-4/+8 |
|
Radar: |
Northrop-Grumman AN/APG-66H pulse-Doppler X-band multimode radar. |
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Centerline
hardpoints: |
1. |
|
Underwing
hardpoints: |
4. |
|
Wingtip
hardpoints: |
2. |
|
Weapons: |
- Aden 30 mm cannon
with 120 rounds.
- AIM-9L Sidewinder.
- AIM-120 AMRAAM.
- Sky Flash.
- AGM-65 Maverick.
- 9 x 240 kg bombs.
- 9 x 113 kg bombs.
- 5 x 540 kg bombs.
- cluster bombs.
- Paveway II Bombs.
-
SNEB rocket pods.
- Sea Eagle missile.
- Marconi Sting Ray
homing torpedo. |
|
Extra: |
- Reconnaissance pod.
- brake chute. |
|
BAe Hawk 100 & 200
operators: |
|
Abu Dhabi. |
- 18 Hawk 102 |
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Australia. |
- 34 Hawk 127LIF |
|
Bahrain. |
- 6 Hawk 127 |
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Canada. |
- 22 CT-155 Hawk (115) |
|
India. |
- 66 Hawk 115 (Hawk AJT)* |
|
Indonesia. |
- 8 Hawk 109
- 32 Hawk 209 |
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Malaysia. |
- 10 Hawk 108
- 18 Hawk 208 |
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Oman. |
- 4 Hawk 103
- 12 Hawk 203 |
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South-Africa. |
- 24 Hawk 120 |
|
United Kingdom. |
- 44 Hawk 128 |
*The intention to procure 66
Hawks (including 42 through local assembly) has been officially confirmed on
several occasions, but due to a variety of reasons no contract has been signed.
British Aerospace Hawk 100 &
Hawk 200 written-off by accidents:
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02jul86 ZG200 Hawk 200 British Aerospace.
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24feb96 1060 Hawk 102 Abu Dhabi
(United Arab Emirates Air Force).
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18jun96 M40-03 Hawk 108 Malaysian Air Force.
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23jul96 M40-10 Hawk 108 Malaysian Air Force.
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10sep98 M40-36 Hawk 208 Malaysian Air Force.
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18jul00 1059 Hawk 102 Abu Dhabi
(United Arab Emirates Air Force).
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18jul00 121 Hawk 203 Royal Air Force of Oman.
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19oct00 TT-104 Hawk 109 Indonesian Air Force.
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16feb01 1056 Hawk 102 Abu Dhabi
(United Arab Emirates Air Force)
16nov01 TT-0201 Hawk 209 Indonesian Air Force.
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31jul02 1057 Hawk 102 Abu Dhabi
(United Arab Emirates Air Force).
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04sep02 M40-35 Hawk 208 Malaysian Air Force.
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14may04 155202 CT-155 Canadian Armed Forces/NFTS.
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22aug04 1064 Hawk 102 Abu Dhabi
(United Arab Emirates Air Force)
Research : R. Vogelaar
Last page-update © zap16.com
11-Oct-2007
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