ST Aerospace A-4SU Super Skyhawk

ST Aerospace A-4SU Super Skyhawk
国	シンガポール共和国
役割	戦闘爆撃機、高度なジェットトレーナー
初飛行	1986年9月19日
構築	150

ザ ST航空宇宙A-4SUスーパースカイホーク は、1980年代にシンガポール航空機産業(SAI、現在ST航空宇宙)が実施したダグラスA-4Sスカイホーク攻撃機の主要なアップグレードプロジェクトです。●1989年から2005年に第一線のサービスから引退するまでの戦闘爆撃機の役割を果たすシンガポール空軍(RSAF)によって独占的に使用されました。1999年半ば以降、A-4SUはフランスのカザウでのRSAFのAJT訓練プログラム/分遣隊の指定高度ジェットトレーナー(AJT)航空機として追加の役割を果たしました。

ソース： ST航空宇宙A-4SUスーパースカイホークオンウィキペディア

TA-4SU Skyhawk Walk Around
カメラマン	Robert Verhegghen
ローカライズ	知りません
写真	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

Click on a photo and use the mouse scroll to view all photos

待って、検索ST航空宇宙A-4SUスーパースカイホーク.

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)
役割	Advanced Jet Trainer / Combat Trainer
National Origin	United States (Original) / Singapore (Upgrade)
メーカー	ST Aerospace (Upgrade)
Service Entry (SU Variant)	1989
乗組員	2 (Student and Instructor)
Length Overall	Approx. 13.10 m (43 ft) (Longer than single-seater due to plug)
翼	8.38 m (27 ft 6 in)
高さ	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.