Difference between revisions of "Banyan S-11"
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| − | {{Short description| | + | {{Short description|Baltanese air superiority fighter}} |
| − | |||
{|{{Infobox aircraft begin | {|{{Infobox aircraft begin | ||
| − | | name = | + | | name = S-11 |
| image = File:Chinese-j-11.jpg | | image = File:Chinese-j-11.jpg | ||
| caption = | | caption = | ||
}}{{Infobox aircraft type | }}{{Infobox aircraft type | ||
| type = [[Air superiority fighter]] | | type = [[Air superiority fighter]] | ||
| − | | manufacturer = [[ | + | | manufacturer = [[Banyan Aircraft Corporation]] |
| designer = | | designer = | ||
| − | | first flight = [[ | + | | first flight = [[1995 in aviation|1995]] |
| − | | introduced = | + | | introduced = 1996 |
| retired = | | retired = | ||
| status = Active service | | status = Active service | ||
| primary user = [[Baltanese Air Force]] | | primary user = [[Baltanese Air Force]] | ||
| − | | more users = <!--up to three more. please separate with <br/>.--> | + | | more users = [[New Illyrian Air Force]] <!--up to three more. please separate with <br/>.--> |
| produced = 1998–present | | produced = 1998–present | ||
| number built = 440 | | number built = 440 | ||
| developed from = [[AR-27]] | | developed from = [[AR-27]] | ||
| variants with their own articles = | | variants with their own articles = | ||
| − | | developed into = [[Banyan | + | | developed into = [[Banyan S-15]] |
| − | [[Banyan | + | [[Banyan S-16]] |
}} | }} | ||
|} | |} | ||
| − | The '''Banyan S-11''' is a [[twinjet|twin-engine]] [[fighter aircraft|jet fighter]] of the [[Baltanla|Federal States of Baltanla]] whose [[airframe]] is derived from the [[Akvarelian]]-designed [[AR-27]]. It is manufactured by the [[Banyan Aircraft Corporation]] (BAC). The aircraft is operated by the [[Baltanese Air Force]] (BAF) | + | The '''Banyan S-11''' is a [[twinjet|twin-engine]] [[fighter aircraft|jet fighter]] of the [[Baltanla|Federal States of Baltanla]] whose [[airframe]] is derived from the [[Akvarelian]]-designed [[AR-27]]. It is manufactured by the [[Banyan Aircraft Corporation]] (BAC). The aircraft is operated by the [[Baltanese Air Force]] (BAF) and the [[New Illyrian Air Force]] (NIAF) |
| + | ==Specifications (S-11A/S-11)== | ||
| + | {{Aircraft specs | ||
| + | <!-- | ||
| + | General characteristics | ||
| + | --> | ||
| + | |crew=1 | ||
| + | |length m=21.9 | ||
| + | |length note= | ||
| + | |span m=14.7 | ||
| + | |span note= | ||
| + | |height m=5.92 | ||
| + | |height note= | ||
| + | |wing area sqm=52.84 | ||
| + | |wing area note= | ||
| + | |aspect ratio=<!-- sailplanes --> | ||
| + | |airfoil= | ||
| + | |empty weight kg=16380 | ||
| + | |empty weight note= | ||
| + | |gross weight kg=23926 | ||
| + | |gross weight note= | ||
| + | |max takeoff weight kg=33000 | ||
| + | |max takeoff weight note= | ||
| + | |fuel capacity={{cvt|9400|kg}} internal fuel | ||
| + | |more general= | ||
| + | |eng1 number =2 | ||
| + | |eng1 name=[[Banyan WS-10A]] "Laoas" | ||
| + | |eng1 type=afterburning turbofans | ||
| + | |eng1 kn=132 | ||
| + | |eng1 note= | ||
| + | |||
| + | <!-- | ||
| + | Performance | ||
| + | --> | ||
| + | |max speed kmh= | ||
| + | |max speed note= | ||
| + | |max speed mach=2.35 (2,500 km/h, 1,553 mph) at altitude | ||
| + | |cruise speed kmh= | ||
| + | |cruise speed note= | ||
| + | |stall speed kmh= | ||
| + | |stall speed note= | ||
| + | |never exceed speed kmh= | ||
| + | |never exceed speed note= | ||
| + | |minimum control speed kmh= | ||
| + | |minimum control speed note= | ||
| + | |range km=3530 | ||
| + | |range note= | ||
| + | |combat range km=1500 | ||
| + | |combat range note= | ||
| + | |ferry range km= | ||
| + | |ferry range note= | ||
| + | |endurance=<!-- if range unknown --> | ||
| + | |ceiling m=19000 | ||
| + | |ceiling note= | ||
| + | |g limits=<big>+</big>9 | ||
| + | |roll rate=<!-- aerobatic --> | ||
| + | |climb rate ms=300 | ||
| + | |climb rate note= | ||
| + | |time to altitude= | ||
| + | |wing loading kg/m2= | ||
| + | |wing loading note= | ||
| + | |fuel consumption kg/km= | ||
| + | |thrust/weight= | ||
| + | |more performance=<!--</br> | ||
| + | *'''Take-off run:''' {{cvt||m|0}} | ||
| + | *'''Take-off run to {{cvt|15|m|0}}:''' {{cvt||m|0}} | ||
| + | *'''Landing run:''' {{cvt||m|0}} | ||
| + | *'''Landing run from {{cvt|15|m|0}}:''' {{cvt||m|0}}--> | ||
| + | <!-- | ||
| + | Armament | ||
| + | --> | ||
| + | |guns=1× 30 mm (1.18 in) [[Quoc-Vao QSh-30-1]] [[autocannon|cannon]] with 150 rounds | ||
| + | |hardpoints=10: 2 under fuselage, 2 under air ducts, 4 under wings, 2 on wingtips | ||
| + | |hardpoint missiles=<br> | ||
| + | ***[[BA-15]] (Later B models and S-11D only) | ||
| + | ***[[BA-12]] | ||
| + | ***[[BA-10]] (Later B and D models) | ||
| + | ***[[BA-9]] | ||
| + | ***[[BA-8 missile|PL-8]] | ||
| + | ***[[Vympel R-77]] | ||
| + | ***[[Vympel R-27]] | ||
| + | ***[[Vympel R-73]] | ||
| + | |bombs=Free-fall [[cluster bombs]] | ||
| + | |rockets=[[Rocket launcher#Rocket pod|Unguided rocket launcher]] | ||
| + | |avionics= | ||
| + | *'''Fire-control radar:''' NIIP Tikhomirov N001VE Myech coherent pulse Doppler radar, or Type 1474 radar (s-11B) | ||
| + | *OEPS-27 electro-optic system | ||
| + | *NSts-27 helmet-mounted sight (HMS) | ||
| + | *Gardeniya ECM pods | ||
| + | }} | ||
| + | [[Category:Terraconserva]] | ||
| + | [[Category:Aircraft]] | ||
| + | [[Category:Baltanla]] | ||
Latest revision as of 00:59, 24 January 2024
| S-11 | |
|---|---|
| |
Role
|
Air superiority fighter |
Manufacturer
|
Banyan Aircraft Corporation |
First flight
|
1995 |
Introduction
|
1996 |
Status
|
Active service |
Primary users
|
Baltanese Air Force New Illyrian Air Force |
Produced
|
1998–present |
Number built
|
440 |
Developed from
|
AR-27 |
Developed into
|
Banyan S-15 |
The Banyan S-11 is a twin-engine jet fighter of the Federal States of Baltanla whose airframe is derived from the Akvarelian-designed AR-27. It is manufactured by the Banyan Aircraft Corporation (BAC). The aircraft is operated by the Baltanese Air Force (BAF) and the New Illyrian Air Force (NIAF)
Specifications (S-11A/S-11)
General characteristics
- Crew: 1
- Fuel capacity: 9,400 kg (20,700 lb) internal fuel
Performance
- Maximum speed: Mach 2.35 (2,500 km/h, 1,553 mph) at altitude
- g limits: +9
Armament
- Guns: 1× 30 mm (1.18 in) Quoc-Vao QSh-30-1 cannon with 150 rounds
- Hardpoints: 10: 2 under fuselage, 2 under air ducts, 4 under wings, 2 on wingtips with provisions to carry combinations of:
- Missiles:
- BA-15 (Later B models and S-11D only)
- BA-12
- BA-10 (Later B and D models)
- BA-9
- PL-8
- Vympel R-77
- Vympel R-27
- Vympel R-73
- Missiles:
- Rockets: Unguided rocket launcher
- Bombs: Free-fall cluster bombs
Avionics
- Fire-control radar: NIIP Tikhomirov N001VE Myech coherent pulse Doppler radar, or Type 1474 radar (s-11B)
- OEPS-27 electro-optic system
- NSts-27 helmet-mounted sight (HMS)
- Gardeniya ECM pods
