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The Boeing
(former McDonnell Douglas) T-45A Goshawk is the
US Navy's two-seat advanced jet trainer. The
aircraft is jointly manufactured by Boeing and
BAE Systems. The T-45A was selected to meet the
US Navy requirement for an undergraduate jet
pilot trainer to replace the TA-4J Skyhawk and
T-2C Buckeye. The TA-4J was retired in 2003 and
the T-2 will be retired in September 2004.The
T-45A entered service with the US Navy in
January 1992. From aircraft number 84 (first
flown on October 21, 1997), production switched
to the T-45C variant, which features a new
"Cockpit 21" with two 5-inch square monochrome
CRT screens. The US Navy and Marine Corps have
more than 160 T-45 Goshawks and a total of 234
is planned. The T-45TS pilot training scheme
includes advanced simulators and computer
assisted instruction as well as training flight
programs.
Several
modifications to the basic Hawk airframe were
incorporated into the T-45 Goshawk design
including: new twin nose-wheel with catapult
launch T-bar; nose wheel steering for
maneuvering within the confines of the carrier
deck; strengthened airframe and undercarriage
for catapult launches; relocated speed brakes;
provision of under-fuselage tail hook; revised
avionics; and modified cockpit layout for
compatibility with frontline US Navy combat
aircraft. |
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Developing nation: |
United
Kingdom/United States. |
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Designer: |
British
Aerospace/McDonnell Douglas. |
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Manufacturer: |
Boeing. |
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Production line: |
St. Louis, MO
USA. |
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Task: |
Lead-in
fighter/carrier trainer. |
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First flight: |
- T-45A April 21,
1998.
- T-45C October
21, 1997. |
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First delivery: |
October 1990 to
Naval Air Test Center at Patuxent River. |
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First carrier
landing: |
December 4, 1991
on the USS John F. Kennedy. |
|
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McDonnell
Douglas/British Aerospace T-45A Goshawk. |
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Crew: |
2.
|
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Ejection seat: |
Martin Baker
Mk.14 NACES. |
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Wing Span: |
9,39 m. |
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Wing Area: |
16,69 m˛. |
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Length fuselage: |
11,17 m. |
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Length fuselage including
probe: |
11,97 m. |
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Height: |
4,27 m. |
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Tail plane span: |
4,59 m. |
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Wheelbase: |
4,29 m. |
|
Wheel track: |
3,90 m. |
|
Engines: |
One Rolls Royce/Turboméca
F405-RR-401 turbofan rated 26.00 kN. |
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Weight: |
- Empty: 4.263 Kg.
- Internal
fuel: 1.312 kg.
- External
fuel: 2 x 591 liter drop tanks. |
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Max. take off weight: |
5.787 Kg. |
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Max. speed: |
997 km/h
at 2.440 m.
|
|
Service ceiling: |
12.875 m. |
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Range: |
1.854 km without
drop tanks. |
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Performance: |
- max. rate of climb
at sea level 2.128 m per minute.
- take-off run to
15 m at max. take-off weight 1.189 m.
- landing run
from 15 m at max. landing weight 1.009 m. |
|
g limits: |
-3/+7.33 |
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Centerline
hardpoints: |
1. |
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Underwing
hardpoints: |
4. |
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Weapons: |
Normally
none, but light stores capability on two wing
and one fuselage pylon. |
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Extra: |
arrester-hook. |
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BAe Hawk
operators: |
|
Abu Dhabi. |
- 1 Hawk
T.63
- 15 Hawk
T.63A
- 5 Hawk T.63C |
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Dubai. |
- 9 Hawk T.61 |
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Finland. |
- 57 Hawk Mk.57 |
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Indonesia. |
- 20 Hawk T.53 |
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Kenya. |
- 12 Hawk T.52 |
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Kuwait. |
- 12 Hawk T.64 |
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Saudi Arabia. |
- 30 Hawk T.65
- 20 Hawk T.65A |
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South-Korea. |
- 20 Hawk T.67 |
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Switzerland. |
- 20 Hawk T.66 |
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United Kingdom. |
- 176 Hawk T.1
(88 T.1s upgraded
with Sidewinder capability to T.1A and 24 to
T.1W). |
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Zimbabwe. |
- 8 Hawk T.60
- 5 Hawk T.60A |
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US Navy. |
- 83 T-45A
Goshawk
- 91 T-45C
Goshawk |
Mc Donnell Douglas T-45
Goshawk written-off by accidents: |
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04-06-1992 |
163601 |
T-45A |
US Navy. |
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17-08-1994 |
163629 |
T-45A |
US Navy. |
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17-08-1994 |
163639 |
T-45A |
US Navy. |
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17-03-1996 |
163627 |
T-45A |
US Navy. |
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01-11-1996 |
163627 |
T-45A |
US Navy. |
|
15-04-1997 |
163634 |
T-45A |
US Navy. |
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11-12-1997 |
163640 |
T-45A |
US Navy. |
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19-08-1998 |
163632 |
T-45A |
US Navy. |
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21-02-2001 |
163601 |
T-45A |
US Navy. |
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08-02-2004 |
165631 |
T-45A |
US Navy. |
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12-07-2004 |
165... |
T-45C |
US Navy. |
|
22-03-2005 |
165... |
T-45C |
US Navy. |
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