ST Aerospace A-4SU Super Skihavk - Fotografije i video

ST Aerospace A-4SU Super Skyhawk
Zemlja	Republika Singapur
Ulogu	Lovac-bombarder, Napredni mlazni trener
Prvi let	19. septembar 1986.
Izgradio	150

Čaj ST Aerospace A-4SU Super Skyhawk je veliki projekat nadogradnje Douglas A-KSNUMKSS Skihavk jurišnog aviona preduzete od strane Singapore Aircraft Industries (SAI, sada ST Aerospace) u KSNUMKSs. Korišćen je isključivo od strane vazduhoplovstva Republike Singapura (RSAF), služeći u ulozi lovca-bombardera od 1989. do penzionisanja iz službe na prvoj liniji 2005. godine. Od sredine KSNUMKS, A-KSNUMKSSU je preuzeo dodatnu ulogu kao određen napredni mlazni trener (AJT) avion za RSAF je AJT program obuke / odreda u Cazauk, Francuska.

Izvor: ST Aerospace A-4SU Super Skyhawk on Wikipedia

TA-4SU Skyhawk Walk Around
Fotograf	Robert Verhegghen
Lokalizacija	Nepoznato
Fotografije	67

TA-4SU Skyhawk 01

TA-4SU Skyhawk 02

TA-4SU Skyhawk 03

TA-4SU Skyhawk 04

TA-4SU Skyhawk 05

TA-4SU Skyhawk 06

TA-4SU Skyhawk 07

TA-4SU Skyhawk 08

TA-4SU Skyhawk 09

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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)
Ulogu	Advanced Jet Trainer / Combat Trainer
National Origin	United States (Original) / Singapore (Upgrade)
Proizvođača	ST Aerospace (Upgrade)
Service Entry (SU Variant)	1989
Posada	2 (Student and Instructor)
Length Overall	Approx. 13.10 m (43 ft) (Longer than single-seater due to plug)
Raspon krila	8.38 m (27 ft 6 in)
Visina	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.