FORCETALLY
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At a glance
Measured figures
DART-450, utility (reconnaissance · Length
Single source10.75 m (35 ft 3 in)[source]
Configuration
| Specification | Diamond DART series | Guizhou JL-9 |
|---|---|---|
| Type | Two-seat military training aircraft[source] | Advanced jet trainer Light combat aircraft[source] |
| National origin | Austria[source] | — |
| Manufacturer | Diamond Aircraft[source] | Guizhou Aviation Industry Import/Export Company (GAIEC)[source] |
| First flight | 17 May 2016 (DART 450)[source] | 13 December 2003[source] |
FTC-2000 · excluding nose-probe
14.555 m (47 ft 9 in) excluding nose-probe[source]
Empty; DART-450, utility (reconnaissance · Empty weight
Single sourceMaximum take-off; DART-450, utility (reconnaissance · Max takeoff weight
Single source1,330 kg (2,932 lb)[source]
2,300 kg (5,071 lb)[source]
Gross; FTC-2000 · clean
Single sourceMaximum take-off; FTC-2000 · Max takeoff weight
Single sourceCruise; DART-450, utility (reconnaissance · Cruise speed
Single sourceMaximum; DART-450, utility (reconnaissance · Maximum speed
Single source460 km/h (290 mph, 250 kn)[source]
430 km/h (260 mph, 230 kn)[source]
Cruise; FTC-2000 · Cruise speed
Single sourceMaximum; FTC-2000 · / Mach 0.89
Single sourceDART-450, utility (reconnaissance · 30 min reserves
Single source2,800 km (1,700 mi, 1,500 nmi) 30 min reserves[source]
DART-450, utility (reconnaissance · 1 × Ivchenko-Progress Motor Sich AI-450S turboprop
Single source1 × Ivchenko-Progress Motor Sich AI-450S turboprop, 369 kW (495 hp)[source]
FTC-2000 · 1 × Guizhou Liyang WP-13F (C) afterburning turbojet thrust dry
Single sourceFTC-2000 · thrust dry and
Single sourceFTC-2000 · with afterburner
Single sourceFTC-2000 · with afterburner (1 × WP-14C Kunlun-3 for FTC-2000G
Single source1 × Guizhou Liyang WP-13F (C) afterburning turbojet, 43.15 kN (9,700 lbf) thrust dry, 63.25 kN (14,220 lbf) with afterburner (1 × WP-14C Kunlun-3 for FTC-2000G, 53.89 kN (12,110 lbf) thrust dry and 76.53 kN (17,200 lbf) with afterburner.)[source]
FTC-2000 · Wing area
Single source26.15 m 2 (281.5 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Developed into | UZGA UTS-800[source] | — |
|---|
| Fuel capacity | 850 L (190 imp gal; 220 US gal) usable[source] | 2,000 kg (4,409 lb) internal + up to 1,302 kg (2,870 lb) in external tanks[source] |
|---|
| Propellers | 5-bladed MT Propeller[source] | — |
|---|
| Stall speed | 110 km/h (69 mph, 60 kn)[source] | 125 km/h (78 mph, 67 kn)[source] |
|---|
| g limits | +7/-4G[source] | + 8 - 3[source] |
|---|
| Take-off run | 600 m (2,000 ft)[source] | 400–500 m (1,300–1,600 ft)[source] |
|---|
| Landing run | 400 m (1,300 ft)[source] | 700 m (2,300 ft)[source] |
|---|
| fuel burn | 90 litres/hour[source] | — |
|---|
| operating cost | $500/hour[source] | — |
|---|
| Designer | — | Aero Engine Research Institute of Guizhou Aviation Industry Corporation[source] |
|---|
| Status | — | In service[source] |
|---|
| Primary users | — | People's Liberation Army Air Force People's Liberation Army Navy Air Force Myanmar Air Force Sudanese Air Force[source] |
|---|
| Developed from | — | Chengdu JJ-7[source] |
|---|
| Guns | — | 1 × 23 mm cannon[source] |
|---|
| Hardpoints | — | 5 with a capacity of 2,000 kg (4,409 lb) maximum, with provisions to carry combinations of: Other: up to 3 x fuel tanks[source] |
|---|
| Unstick and touchdown speed | — | 260 km/h (160 mph; 140 kn)[source] |
|---|
| Minimum flying speed | — | 210 km/h (130 mph; 110 kn)[source] |
|---|
| Wing loading | — | 374.8 kg/m 2 (76.8 lb/sq ft)[source] |
|---|
| Thrust/weight | — | 0.00645 kN/kg (0.658 lb f /lb)[source] |
|---|
| Other | — | up to 3 x fuel tanks[source] |
|---|
| Missiles | — | ** Short range air-to-air missile 2 × PL-8 AAMs (on inboard pylons) 2 × PL-9 AAMs (on outboard pylons) Beyond-visual-range air-to-air missiles SD-10 (Only on FTC-2000G) Anti-radiation missiles CM-102 (Only on FTC-2000G)[source] |
|---|
| Beyond-visual-range air-to-air missiles | — | SD-10 (Only on FTC-2000G)[source] |
|---|
| Anti-radiation missiles | — | CM-102 (Only on FTC-2000G)[source] |
|---|
| Country of origin | — | Volksrepublik China[source]Country of design · Entwurfsland |
|---|
| Reported operators |
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