Cheppali GF-19 Garuda: Difference between revisions
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Many of the aircraft’s avionics and features take advantage of the work carried out on the GF-20 Berunda and expand upon it. Some features that were included during development were direct voice input, AESA radar, and an integrated IRST sensor. The aircraft is available in two main variants: Garuda A twin-seat land based version and the Garuda B twin-seat carrier-based version. | Many of the aircraft’s avionics and features take advantage of the work carried out on the GF-20 Berunda and expand upon it. Some features that were included during development were direct voice input, AESA radar, and an integrated IRST sensor. The aircraft is available in two main variants: Garuda A twin-seat land based version and the Garuda B twin-seat carrier-based version. | ||
==Specifications== | ==Specifications (Garuda A)== | ||
{{Aircraft specs | |||
|prime units?=met | |||
<!-- | |||
General characteristics | |||
--> | |||
|crew=2 | |||
|length m=18.7 | |||
|length note= | |||
|span m=12 | |||
|span note= | |||
|height m=5.8 | |||
|height note= | |||
|wing area sqm=73 | |||
|wing area note= | |||
|aspect ratio=<!-- sailplanes --> | |||
|airfoil=<!--'''root:''' [[NACA airfoil|NACA ]]; '''tip:''' [[NACA airfoil|NACA ]]<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |accessdate=16 April 2019}}</ref>--> | |||
|empty weight kg=13000 | |||
|empty weight note= | |||
|gross weight kg=16100 | |||
|gross weight note= | |||
|max takeoff weight kg= | |||
|max takeoff weight note= | |||
|fuel capacity= | |||
|more general= | |||
<!-- | |||
Powerplant | |||
--> | |||
|eng1 number=2 | |||
|eng1 name=[[Gikrabanda G1120-229]] | |||
|eng1 type=afterburning [[turbofan]] | |||
|eng1 kn=<!-- jet/rocket engines --> | |||
|eng1 lbf= | |||
|eng1 note= | |||
|eng1 kn-ab=130 | |||
<!-- | |||
Performance | |||
--> | |||
|max speed kmh=2901.78 | |||
|max speed note= | |||
|max speed mach= 2.35 | |||
|cruise speed kmh= | |||
|cruise speed note= | |||
|stall speed kmh= | |||
|stall speed note= | |||
|never exceed speed kmh= | |||
|never exceed speed note= | |||
|range km=4000 | |||
|range note= | |||
|combat range km=2000 | |||
|combat range note= | |||
|ferry range km=10000 | |||
|ferry range note= | |||
|endurance=<!-- if range unknown --> | |||
|ceiling m=20000 | |||
|ceiling note= | |||
|g limits=<!-- aerobatic --> | |||
|roll rate=<!-- aerobatic --> | |||
|climb rate ms=350 | |||
|climb rate note= | |||
|time to altitude= | |||
|wing loading kg/m2=220 | |||
|wing loading note= | |||
|fuel consumption kg/km= | |||
|thrust/weight=1.34 | |||
|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 caliber|30 mm]] [[Kala cannon]] | |||
|hardpoints= 12 total;6 × under-wing, and 6× under-fuselage pylon stations | |||
|hardpoint capacity=up to {{convert|9000|kg|lb|abbr=on}} of stores | |||
|rockets=<br> | |||
**4 x rocket pods (each with 19 x 70 mm rockets) | |||
**4 x rocket pods (each with 4 x 217 mm rockets) | |||
|missiles=<br> | |||
** [[Air-to-air missile]]s: | |||
***[[Katteri-7 MRMS]] | |||
***[[Katteri-9 SRMS]] | |||
***[[Katteri-120 ALRMS]] | |||
***[[Steel Arrow VADMS]] | |||
***[[Viper (missile)|Viper-4]] | |||
***[[Viper (missile)|Viper-5]] | |||
** [[Air-to-surface missile]]s: | |||
***[[AGM-65 Koḷḷaikkāraṉ]] | |||
***[[AGM-88 ARMS]] | |||
*** [[AGM-158 JASSM]] | |||
***[[AGM-154 Joint Standoff Weapon]] | |||
** [[Anti-ship missile]]s: | |||
***[[Boeing Harpoon|Boeing Harpoon]] | |||
***[[Penguin missile|Penguin missile]] | |||
|bombs=<br> | |||
**[[CBU-87 Combined Effects Munition]] | |||
**[[GATOR mine system|CBU-89 Gator mine]] | |||
**[[CBU-97 Sensor Fuzed Weapon]] | |||
**[[Mark 84 bomb|Mark 84]] | |||
**[[Mark 83 bomb|Mark 83]] | |||
**[[Mark 82 bomb|Mark 82]] | |||
**[[GBU-39 SDB|GBU-39 Small Diameter Bomb]] | |||
**[[GBU-10 Paveway II]] | |||
**[[GBU-12 Paveway II]] | |||
**[[GBU-24 Paveway III]] | |||
**[[GBU-27 Paveway III]] | |||
**[[Joint Direct Attack Munition]] | |||
** [[Wind Corrected Munitions Dispenser]] | |||
** [[B61 nuclear bomb]] | |||
** [[B83 nuclear bomb]] | |||
*'''Others:''' | |||
**SUU-42A/A [[Flare (countermeasure)|Flares/Infrared decoys]] dispenser pod and [[chaff (radar countermeasure)|chaff]] pod ''or'' | |||
**AN/ALQ-131 & AN/ALQ-184 [[electronic countermeasures|ECM]] pods ''or'' | |||
** [[LANTIRN]], [[Lockheed Martin Sniper XR]] & [[LITENING targeting pod]]s ''or'' | |||
**Up to 3 × 660 US gallon drop tanks for ferry flight/extended range/loitering time | |||
|avionics= | |||
*ML/M-2052 AESA radar | |||
*ACE-6 computer | |||
*Razor 112 Helmet-mounted display system | |||
}} |
Revision as of 14:02, 16 August 2020
GF-29 Garuda | |
---|---|
Role | Multirole fighter |
Manufacturer | Cheppali International |
First flight | 20 April 1990 |
Introduction | 9 July 1995 |
Status | In active service |
Primary user | Tennai |
Program cost | US$2 billion |
Unit cost |
$25 million
|
The Cheppali International GF-19 Garuda is a Tennaiite twin-engine, all-weather multirole fighter designed and built by Cheppali International. Equipped with a wide range of weapons, the Garuda is intended to perform air supremacy, interdiction, aerial reconnaissance, in-depth strike, anti-ship strike and nuclear deterrence missions.
Many of the aircraft’s avionics and features take advantage of the work carried out on the GF-20 Berunda and expand upon it. Some features that were included during development were direct voice input, AESA radar, and an integrated IRST sensor. The aircraft is available in two main variants: Garuda A twin-seat land based version and the Garuda B twin-seat carrier-based version.
Specifications (Garuda A)
General characteristics
- Crew: 2
- Length: 18.7 m (61 ft 4 in)
- Wingspan: 12 m (39 ft 4 in)
- Height: 5.8 m (19 ft 0 in)
- Wing area: 73 m2 (790 sq ft)
- Empty weight: 13,000 kg (28,660 lb)
- Gross weight: 16,100 kg (35,494 lb)
- Powerplant: 2 × Gikrabanda G1120-229 afterburning turbofan, 130 kN (29,000 lbf) with afterburner
Performance
- Maximum speed: 2,901.78 km/h (1,803 mph; 1,567 kn)
- Maximum speed: Mach 2.35
- Range: 4,000 km (2,485 mi; 2,160 nmi)
- Combat range: 2,000 km (1,243 mi; 1,080 nmi)
- Ferry range: 10,000 km (6,214 mi; 5,400 nmi)
- Service ceiling: 20,000 m (66,000 ft)
- Rate of climb: 350 m/s (69,000 ft/min)
- Wing loading: 220 kg/m2 (45 lb/sq ft)
- Thrust/weight: 1.34
Armament
- Guns: 1 × 30 mm Kala cannon
- Hardpoints: 12 total;6 × under-wing, and 6× under-fuselage pylon stations with a capacity of up to 9,000 kg (20,000 lb) of stores,
- Rockets:
- 4 x rocket pods (each with 19 x 70 mm rockets)
- 4 x rocket pods (each with 4 x 217 mm rockets)
- Missiles:
- Bombs:
- CBU-87 Combined Effects Munition
- CBU-89 Gator mine
- CBU-97 Sensor Fuzed Weapon
- Mark 84
- Mark 83
- Mark 82
- GBU-39 Small Diameter Bomb
- GBU-10 Paveway II
- GBU-12 Paveway II
- GBU-24 Paveway III
- GBU-27 Paveway III
- Joint Direct Attack Munition
- Wind Corrected Munitions Dispenser
- B61 nuclear bomb
- B83 nuclear bomb
- Others:
- SUU-42A/A Flares/Infrared decoys dispenser pod and chaff pod or
- AN/ALQ-131 & AN/ALQ-184 ECM pods or
- LANTIRN, Lockheed Martin Sniper XR & LITENING targeting pods or
- Up to 3 × 660 US gallon drop tanks for ferry flight/extended range/loitering time
Avionics
- ML/M-2052 AESA radar
- ACE-6 computer
- Razor 112 Helmet-mounted display system