You never know what a change in government and a new defence review white paper can accomplish. The USAF favors this aircraft to replace its T-38 Talons over the T-45 Goshawk. Its not a F-16, but its better than nothing! At $20 million each, its more expensive than the Goshawk, which is now running $15 million each. These are US dollars. At NZ $40 million each, 20 could be acquired for NZ $800 million. Increase the acquisition budget $100 million a year, and you'll have them, the GDP increase in defence spending would be approximately .2 percent. From 1.0 to 1.2 GDP.
Some specs for the T-50 Golden Hawk from an airforce website:
Length 12.98m
Height 4,78m
Wingspan 9.11m
Wingspan including missiles 9.17m
Empty weight 6,263kg
Maximum take-off weight without external payload 8,890kg
Maximum take-off weight with external payload 11,974kg
Type 1 x General Electric F404-102 turbofan
Engine length 4,030mm
Engine diameter 880mm
Engine dry weight 1,035kg
Take-off power rating 78.7kN (17700 lbs)
Maximum level speed Mach 1.45
Maximum altitude 14,500m
Manoeuvrability +8g to -3g
Max. climb rate 201 m/s
Time of climb
To 10000 ft 56 sec
To 20000 ft 74 sec
To 30000 ft 102 sec
Takeoff distance 345 m
Landing distance 707 m on a standard day
Range 2600 km, clean, with external tanks and 10 per cent reserve
Typical mission duration 146 min, with 74 min in the air work area.
Service life 8300 h
COCKPIT: The aircraft has digital fly-by-wire controls and HOTAS (Hands On Throttle And Stick). The cockpit displays include two 127mm full colour Honeywell multifunction displays, Honeywell instrumentation displays and a Head Up Display (HUD) supplied by BAE Systems.
The full authority digital flight control system and avionics were developed by Lockheed Martin Aeronautics Division at Fort Worth. The flight equipment includes a navigation / attack system, a Honeywell H-764G embedded global positioning / inertial navigation system and HG9550 radar altimeter, Rockwell Collins VIR-130A integrated VOR / instrument landing system and ARN-153V advanced digital tactical aid to navigation, and Raytheon ARC-232 VHF radio.
The AN/APG-67(V)4 multi-mode radar, supplied by Lockheed Martin, is installed in the nose of the LIFT version.
The two crew, tandem stepped cockpit is fitted with an onboard oxygen generating system (OBOGS) and ejection seats supplied by Martin Baker of Uxbridge, UK.
WEAPONS: The aircraft has seven external hardpoints for carrying weapons, one on the centreline under the fuselage, two hardpoints under each wing and an air-to-air missile launch rail at the two wingtips.
The wingtip launch rails can carry AIM-9 Sidewinder missiles. The underwing and centreline hardpoints can carry rocket pods, air-to-surface missiles or air-to-air missiles according to the mission requirements, e.g. AGM-65 Maverick missiles or Mark 82/83/84 bombs or rocket launchers.
In November 2005, the A-50 successfully test-fired an AIM-9L air-to-air missile.
A 20mm General Dynamics Armaments three-barrel M61 cannon is installed internally on the A-50 LIFT version. The gun is mounted behind the cockpit and carries 205 rounds of ammunition in a linear linkless feed system. The A-50 LIFT can carry electronic warfare pods and a radar warning receiver.
ENGINES: The aircraft is powered by a single General Electric turbofan engine, type F404-GE-102, with FADEC (Full Authority Digital Electronic Control). It is a derivative of the 402 with additional improvements in the turbine and afterburner. The engine has twin side mounted air intakes on either side of the fuselage under the wing.
The engine, with a three-fan stage and seven axial stage arrangement, is equipped with full authority digital engine control and generates 78.7kN with afterburn.
The aircraft has seven internal fuel tanks, five in the fuselage and two in the wings, which can carry 2,655L of fuel with the option of three additional 570L external fuel tanks.
The aircraft is fitted with an Argo-Tech fuel system. The power generator is supplied by Hamilton Sundstrand.