TA-4SU Skyhawk

ST Aerospace A-4SU Super Skyhawk

RiikSingapuri Vabariik
RolliHävitaja-pommitaja, täiustatud reaktiivtreeninglennuk
Esimene lend19. september 1986
Ehitatud150

2007 ST Aerospace A-4SU Super Skyhawk on Singapore Aircraft Industriesi (SAI, nüüd ST Aerospace) 1980. aastatel ette võetud ründelennuki Douglas A-4S Skyhawk suur uuendusprojekt. Seda kasutasid eranditult Singapuri Vabariigi õhujõud (RSAF), teenides hävitaja-pommitaja rollis alates 1989. aastast kuni rindeteenistusest pensionile jäämiseni 2005. aastal. Alates 1999. aasta keskpaigast võttis A-4SU endale täiendava rolli, olles Prantsusmaal Cazaux's asuva RSAF-i AJT väljaõppeprogrammi/üksuse määratud täiustatud reaktiivtreeninglennuk (AJT).

Allikas: ST Aerospace A-4SU Super Skyhawk Vikipeedias

TA-4SU Skyhawk Walk Around
FotograafRobert Verhegghen
LokaliseerimineTeadmata
Fotod67
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General Characteristics and Upgrade

The TA-4SU Super Skyhawk is the two-seat trainer variant of the A-4SU Super Skyhawk, which was a major modernization of the Douglas A-4S/A-4S-1 Skyhawk attack aircraft carried out by Singapore Technologies Aerospace (ST Aerospace) for the Republic of Singapore Air Force (RSAF) in the late 1980s. The upgrade transformed the aircraft by replacing its original underpowered engine with a modern turbofan and installing advanced avionics. The TA-4SU is unique among Skyhawk trainers, featuring a 710 mm (28 inch) fuselage plug and two completely separate cockpits, each with its own canopy, giving the rear-seat instructor excellent forward visibility. It was used for operational conversion and advanced jet training.

Property Typical Value (TA-4SU Trainer)
Rolli Advanced Jet Trainer / Combat Trainer
National Origin United States (Original) / Singapore (Upgrade)
Tootja ST Aerospace (Upgrade)
Service Entry (SU Variant) 1989
Meeskonna 2 (Student and Instructor)
Length Overall Approx. 13.10 m (43 ft) (Longer than single-seater due to plug)
Tiibade siruulatus 8.38 m (27 ft 6 in)
kõrgus 4.57 m (15 ft 0 in)
Max Takeoff Weight 10,205 kg (22,500 lb)

Powerplant and Performance

  • Engine: One General Electric F404-GE-100D non-afterburning turbofan engine.
  • Thrust: 48.4 kN (10,800 lbf).
    • Note: This replacement improved climb rate by 35% and acceleration by 40% compared to the original J65 turbojet.
  • Maximum Speed: 1,128 km/h (701 mph; 609 knots).
  • Rate of Climb: Approx. 55 m/s (10,913 ft/min).
  • Ferry Range: 3,220 km (2,000 mi) with 3 external drop tanks.
  • Service Ceiling: 12,192 m (40,000 ft).

Armament and Avionics

  • Fixed Armament: 2 x 30 mm ADEN cannons (200 rounds/gun).
  • Hardpoints: 5 total (1 centreline, 4 underwing) with a capacity of 4,500 kg (9,900 lb).
  • Ordnance Capability: Can carry a variety of munitions, including:
    • Air-to-Air Missiles: AIM-9 Sidewinder.
    • Air-to-Surface Missiles: AGM-65 Maverick.
    • Bombs: Paveway Laser-Guided Bombs (LGBs) and Mark 80 series unguided bombs.
  • Avionics Upgrade: The suite includes a GEC/Ferranti 4510 Head-up display (HUD), Litton LN-93 Inertial Navigation System (INS), and multi-function displays.
  • Trainer Feature: Fully capable of weapons delivery, serving as a combat trainer, unlike many other two-seat trainers.

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