Difference between revisions of "Arlert Ar-85"
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− | The '''Arlert Ar-85''' is a Akvarelian-origin twin-engine supermaneuverable fighter aircraft designed by [[Arlert]]. It servs as the bases for the [[Arlert Ar-14/2]] and [[Arlert Ar-96]]. Furthermore the [[Banyan S-16]] is the | + | The '''Arlert Ar-85''' is a Akvarelian-origin twin-engine supermaneuverable fighter aircraft designed by [[Arlert]]. It servs as the bases for the [[Arlert Ar-14/2]] and [[Arlert Ar-96]]. Furthermore the [[Banyan S-16]] is the Baltanese version of the plane. [[TF-30 Guardian]] is the Ar-85 build under license in [[Abersiania]] |
== Specifications (Ar-85) == | == Specifications (Ar-85) == | ||
[[File:Sukhoi Su-27 3-view line drawing.svg|thumb|Arlert Ar-85 3-view drawings]] | [[File:Sukhoi Su-27 3-view line drawing.svg|thumb|Arlert Ar-85 3-view drawings]] |
Latest revision as of 10:41, 22 April 2024
Ar-85 | |
---|---|
Ar-85 in flight | |
Role
|
Multirole fighter, air superiority fighter |
National origin
|
Akvarelusus |
Manufacturer
|
JSC Arlert |
First flight
|
20 May 1977 |
Introduction
|
22 June 1985 |
Status
|
in use |
Primary user
|
|
Produced
|
1982-present |
Number built
|
140 |
Unit cost
|
₵ 30 000 000 QSC
|
Developed from
|
Arlert Panda |
The Arlert Ar-85 is a Akvarelian-origin twin-engine supermaneuverable fighter aircraft designed by Arlert. It servs as the bases for the Arlert Ar-14/2 and Arlert Ar-96. Furthermore the Banyan S-16 is the Baltanese version of the plane. TF-30 Guardian is the Ar-85 build under license in Abersiania
Specifications (Ar-85)
General characteristics
- Crew: 1
- Length: 21.9 m (71 ft 10 in)
- Wingspan: 14.7 m (48 ft 3 in)
- Height: 5.92 m (19 ft 5 in)
- Wing area: 62 m2 (670 sq ft)
- Empty weight: 16,380 kg (36,112 lb)
- Gross weight: 23,430 kg (51,654 lb)
- Max takeoff weight: 30,450 kg (67,131 lb)
- Fuel capacity: 9,400 kg (20,723.5 lb) internal dry, 122.6 kN (27,600 lbf) with afterburner
Performance
- Maximum speed: 2,500 km/h (1,600 mph, 1,300 kn) / M2.35 at altitude
- 1,400 km/h (870 mph; 760 kn) / M1.13 at sea level
- Range: 3,530 km (2,190 mi, 1,910 nmi) At altitude
- 1,340 km (830 mi; 720 nmi) at sea level
- Service ceiling: 19,000 m (62,000 ft)
- g limits: +9
- Rate of climb: 300 m/s (59,000 ft/min)
- Wing loading: 377.9 kg/m2 (77.4 lb/sq ft) With 56% fuel
- 444.61 kg/m2 (91.1 lb/sq ft)
- Thrust/weight: 1.07 with 56% internal fuel; 0.91 with full fuel
Armament
- Guns: 1 × 30 mm autocannon with 150 rounds
- Hardpoints: 10 external pylons with a capacity of up to 4,430 kg (9,770 lb),