SAI GR-7 Imam Ardashir: Difference between revisions
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{{aircraft specifications | |||
<!-- If you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]]. --> | |||
| plane or copter? = plane | |||
| jet or prop? = jet | |||
<!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item does not apply, like capacity, leave it blank. | |||
--> | |||
| ref = | |||
<!-- General characteristics --> | |||
| crew = 2 | |||
| capacity = | |||
| payload main = | |||
| payload alt = | |||
| payload more = | |||
| length main = 17.53 m | |||
| length alt = 57.5 ft | |||
| span main = 8.69 m | |||
| span alt = 28.6 ft | |||
| height main = 4.89 m | |||
| height alt = 16.1 ft | |||
| area main = | |||
| area alt = | |||
| airfoil = | |||
| aspect ratio = | |||
| empty weight main = 7,000 kg | |||
| empty weight alt = 15,432 lb | |||
| useful load main = | |||
| useful load alt = | |||
| loaded weight main = 10,954 kg | |||
| loaded weight alt = 24,149 lb | |||
| max takeoff weight main = 15,700 kg | |||
| max takeoff weight alt = 34,613 lb | |||
| more general = | |||
<!-- Powerplant, jet engine(s) --> | |||
| engine (jet) = Badyar-1352 | |||
| type of jet = afterburning turbofan | |||
| number of jets = 2 | |||
| thrust main = 22.75 kN | |||
| thrust alt = 5,110 lbf | |||
| thrust original = | |||
| afterburning thrust main = 32.5 kN | |||
| afterburning thrust alt = 7,300 lbf | |||
<!-- Powerplant, prop(s) --> | |||
| engine (prop) = | |||
| type of prop = | |||
| number of props = | |||
| power main = | |||
| power alt = | |||
| power original = | |||
<!-- Powerplant, propellor/rotor details --> | |||
| propeller or rotor? = <!-- options: propeller/rotor --> | |||
| propellers = | |||
| number of propellers per engine = | |||
| propeller diameter main = | |||
| propeller diameter alt = | |||
| more general powerplant = | |||
<!-- Performance --> | |||
| max speed main = Mach 1.1 (at sea level) | |||
| max speed alt = 1,350 km/h (840 mph, 730 kn; at sea level)<br/>1,699 km/h (1,056 mph; 917 kn) Mach 1.6 at 11,000 m (36,000 ft) | |||
| max speed more = | |||
| cruise speed main = | |||
| cruise speed alt = | |||
| cruise speed more = | |||
| stall speed main = | |||
| stall speed alt = | |||
| stall speed more = | |||
| never exceed speed main = | |||
| never exceed speed alt = | |||
| range main = | |||
| range alt = | |||
| range more = | |||
| combat radius main= 800 km<br/> | |||
815 km (506 mi, 440 nmi) hi-lo-hi (internal fuel)<br/>575 km (357 mi; 310 nmi) lo-lo-lo (internal fuel)<br/>1,408 km (875 mi; 760 nmi) hi-lo-hi (with external fuel)<br/>908 km (564 mi; 490 nmi) lo-lo-lo (with external fuel | |||
| combat radius alt = | |||
| combat radius more= | |||
| ferry range main = | |||
| ferry range alt = | |||
| ferry range more = | |||
| endurance = | |||
| ceiling main = 13,500 m | |||
| ceiling alt = 44,291. ft | |||
| ceiling more = | |||
| climb rate main = | |||
| climb rate alt = | |||
| climb rate more = | |||
| sink rate main = | |||
| sink rate alt = | |||
| sink rate more = | |||
| loading main = | |||
| loading alt = | |||
| thrust/weight = | |||
| power/mass main = | |||
| power/mass alt = | |||
| more performance = | |||
<!-- Armament --> | |||
| guns = 2× {{wp|Gryazev-Shipunov GSh-23|MTs-23}} autocannon, 120 rounds each | |||
| bombs = | |||
| rockets = | |||
| missiles = | |||
| hardpoints = 9 in total (6× under-wing, 2× wing-tip, 1× under-fuselage) with a capacity of 9,000 kg (20,000 lb) external fuel and ordnance, | |||
| hardpoint rockets = <br> | |||
***{{wp|UB-32}} rocket pods | |||
***B-8M rocket pods for {{wp|S-8 (rocket)|S-8 rockets}} | |||
***{{wp|S-13 rocket|S-13}} | |||
***{{wp|S-24 rocket|S-24}} | |||
***{{wp|S-25 rocket|S-25}} | |||
| hardpoint missiles = <br> | |||
***{{wp|Air-to-air missile|Air-to-air missiles}}: | |||
****{{wp|K-13 (missile)|K-13A}} | |||
****{{wp|R-60 (missile)|R-60}} | |||
****{{wp|R-73 (missile)|R-73}} | |||
***{{wp|Air-to-surface missile|Air-to-surface missiles}}: | |||
****{{wp|Kh-23 Grom|Kh-23}} | |||
****{{wp|Noor (missile)|Noor}} | |||
****{{wp|Kh-29}} | |||
***{{wp|Anti-radiation missile|Anti-radiation missiles}}: | |||
****{{wp|Kh-28}} | |||
****{{wp|PL-12}} | |||
| hardpoint bombs = <br> | |||
***{{wp|BETAB-500}} | |||
***FAB-250 | |||
***{{wp|FAB-500}} | |||
***FAN-500 | |||
***{{wp|KAB-500KR}} | |||
***ZAB-500 incendiary bomb | |||
| hardpoint other = {{wp|Electronic counter-measures|ECM protection pods}}, Reconnaissance Pod, laser/electro-optical targeting pods, external drop tanks for extended range/loitering time | |||
| avionics = {{wp|JL-10A|QR-10A}} | |||
}} | |||
[[Category:Zorasan]] | [[Category:Zorasan]] | ||
Revision as of 03:10, 4 February 2020
| SAI G-7 Imam Ardashir | |
|---|---|
| |
| A SAI G-7/B on the tarmac | |
| Role | Attack aircraft |
| National origin | Zorasan |
| Manufacturer | Soltanabad Aeronautic Industries |
| Designer | Soltanabad Aerospace Design Institute |
| First flight | 1970 |
| Introduction | 1975 |
| Status | In service |
| Primary user |  Zorasani Irfanic Revolutionary Army Air Force
|
| Produced | 1974-1990 |
| Number built | 266 |
The SAI GR-7 Imam Ardashir (Pasdani: امام اردشیر گر-۷) is a twin-seat attack aircraft used by the Zorasani Irfanic Revolutionary Army Air Force in the close air support role.
Initially designed as a medium-range interceptor, the final design was radically altered to meet the requirements of a domestically produced fighter-bomber, where the ZIRAAF had historically been lacking. Considerable effort was placed into the design and production of the first domestic supersonic capable turbofan engine, this was ultimately achieved with the inception of the Badyar-1352. The final design also saw a strengthened airframe and more hardpoints, to grant the aircraft a significantly larger payload than originally intended.
The GR-7 has seen extensive operational service, proving highly vauled in the Irvadistan War by the ZIRAAF, but also saw action in the Al-Thawra Rebellion, Al-Hizan Uprising, the Kexri Conflict and the 2003-2004 Amardo-Zorasani Standoff. Despite the purchase of 40 Shengkong JK-10 fighter-bombers in 1999, the GR-7 has remained in service, with significant upgrades to its avionics, engine and fuel tank since its introduction in 1974.
Design and development
Design
Overview
Engine
Avionics
Operational history
Zorasan
Specifications
General characteristics
- Crew: 2
- Length: 17.53 m (57.5 ft)
- Wingspan: 8.69 m (28.6 ft)
- Height: 4.89 m (16.1 ft)
- Empty weight: 7,000 kg (15,432 lb)
- Loaded weight: 10,954 kg (24,149 lb)
- Max. takeoff weight: 15,700 kg (34,613 lb)
- Powerplant: 2 × Badyar-1352 afterburning turbofan
- Dry thrust: 22.75 kN (5,110 lbf) each
- Thrust with afterburner: 32.5 kN (7,300 lbf) each
Performance
- Maximum speed: Mach 1.1 (at sea level) (1,350 km/h (840 mph, 730 kn; at sea level)
1,699 km/h (1,056 mph; 917 kn) Mach 1.6 at 11,000 m (36,000 ft)) - Combat radius: 800 km
815 km (506 mi, 440 nmi) hi-lo-hi (internal fuel)
575 km (357 mi; 310 nmi) lo-lo-lo (internal fuel)
1,408 km (875 mi; 760 nmi) hi-lo-hi (with external fuel)
908 km (564 mi; 490 nmi) lo-lo-lo (with external fuel ()
- Service ceiling: 13,500 m (44,291. ft)
Armament
- Guns: 2× MTs-23 autocannon, 120 rounds each
- Hardpoints: 9 in total (6× under-wing, 2× wing-tip, 1× under-fuselage) with a capacity of 9,000 kg (20,000 lb) external fuel and ordnance, and provisions to carry combinations of:
- Rockets:
- UB-32 rocket pods
- B-8M rocket pods for S-8 rockets
- S-13
- S-24
- S-25
- Missiles:
- Bombs:
- Other: ECM protection pods, Reconnaissance Pod, laser/electro-optical targeting pods, external drop tanks for extended range/loitering time
- Rockets:
Avionics
QR-10A