AmirPatriot
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It's possible that Iran would buy 30-40 aircraft, and produce the rest inside the country.
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It's possible that Iran would buy 30-40 aircraft, and produce the rest inside the country.
Pretty much yeah. You realize building a reliable and durable jet engine isnt something that can be done by simply displaying a prototype to the public. ?
Another possibility ... we won't get any Su-30 !
I say more likely than any other possibility.Another possibility ... we won't get any Su-30 !
Another possibility ... we won't get any Su-30 !
Pretty much yeah. You realize building a reliable and durable jet engine isnt something that can be done by simply displaying a prototype to the public. These things needs many years to mature and considering the poor state of Iran's air force there are simply urgent requirements that need to be fullfilled. Plus a lot of military developments in Iran arent matured products, this isnt ment to insult Iranians or Iran but it really is the case. Why do you think Iran is looking for new goodies to purchase?
What are you blagging about? That engine has been testing for 6-10 years. You think what they revealed meant that they only just made it?
I very much doubt that.
Specifications (F-5E Tiger II)
General characteristics
Performance
- Crew: 1
- Length: 47 ft 4¾ in (14.45 m)
- Wingspan: 26 ft 8 in (8.13 m)
- Height: 13 ft 4½ in (4.08 m)
- Wing area: 186 ft² (17.28 m²)
- Airfoil: NACA 65A004.8 root, NACA 64A004.8 tip
- Empty weight: 9,558 lb (4,349 kg)
- Loaded weight: 15,745 lb (7,157 kg)
- Max. takeoff weight: 24,722 lb (11,214 kg)
- Powerplant: 2 × General Electric J85-GE-21B turbojet
- Dry thrust: 3,500 lbf (15.5 kN) each
- Thrust with afterburner: 5,000 lbf (22.2 kN) each
- Zero-lift drag coefficient: 0.0200
- Drag area: 3.4 ft² (0.32 m²)
- Aspect ratio: 3.82
- Internal fuel: 677 U.S. gal (2,563 L)
- External fuel: 275 U.S. gal (1,040 L) per tank in up to 3 tanks
Armament
- Maximum speed: 917 kn (Mach 1.6, 1,060 mph, 1,700 km/h) ; at altitude
- Range: 760 nmi (870 mi, 1,405 km)
- Ferry range: 2,010 nmi (2,310 mi, 3,700 km[171])
- Service ceiling: 51,800 ft (15,800 m)
- Rate of climb: 34,400 ft/min (175 m/s)
- Lift-to-drag ratio: 10.0
Specifications (HESA Saeqeh)
- Guns: 2× 20 mm (0.787 in) M39A2 Revolver cannons in the nose, 280 rounds/gun
- Hardpoints: 7 total (only pylon stations 3, 4 and 5 are wet-plumbed): 2× wing-tip AAM launch rails, 4× under-wing & 1× under-fuselage pylon stations with a capacity of 7,000 pounds (3,200 kg)
General characteristics
Performance
- Crew: 1
- Length: 15.89 m (52 ft 2 in)
- Wingspan: 8.3 m (27 ft 3 in)
- Empty weight: 4,400 kg (9,700 lb)
- Gross weight: 9,000 kg (19,842 lb)
- Powerplant: 2 × unknown afterburning turbojet engines
Armament
- Maximum speed: 1,700 km/h (1,056 mph; 918 kn)
- Maximum speed: Mach 1.4+
- Range: 3,000 km (1,864 mi; 1,620 nmi)
- Service ceiling: 16,000 m (52,493 ft)
- Rate of climb: 175 m/s (34,400 ft/min)
Specifications (Yak-130)
- Guns: 2× 20 mm (0.787 in) M39A2 Revolver cannons in the nose, 280 rounds/gun
- Hardpoints: 7 total: 2× wing-tip AAM launch rails, 4× under-wing & 1× under-fuselage pylon stations with a capacity of 7,000 pounds (3,200 kg)
General characteristics
Performance
- Crew: 2 pilots
- Length: 11.49 m (37 ft 8 in)
- Wingspan: 9.84 m (32 ft 3 in)
- Height: 4.76 m (15 ft 7 in)
- Wing area: 23.52 m² (253.2 sq ft)
- Empty weight: 4,600 kg (10,141 lb)
- Loaded weight: 7,250 kg (15,984 lb) (normal take-off weight)
- Max. takeoff weight: 10,290 kg (22,686 lb)
- Powerplant: 2 × Progress AI-222-25 turbofan, 24.52 KN (5,512 lbf) each
Armament
- Maximum speed: 1,060 km/h (648 mph)
- Cruise speed: 887 km/h (551 mph)
- Stall speed: 165 km/h (103 mph)
- Range: 2,100 km (1,305 miles)
- Combat radius: 555 km (345 miles)
- Service ceiling: 12,500 m (42,660 ft)
- Rate of climb: 65 m/s (10,000 ft/min)
- Wing loading: 276.4 kg/m² (56.60 lb/sq ft)
- Thrust/weight: 0.9
A symmetric or asymmetric weapon load, weighing up to 3,000 kg (6,600 lb) and consisting of various guided and un-guided weapons, auxiliary fuel tanks and electronics pods can be carried on 9 hardpoints: 1 on each wingtip, 3 under each wing, and 1 under the fuselage.
Yakovlev Yak-131
light attack aircraft for Su-25 replacement. This version will have cockpit and engine armour, a GSh-301 gun, and either the Phazotron Kopyo radar with mechanical or electronic beam scanning, or the Tikhomirov NIIP Osa passive phased array radar
I very much doubt that.
Probably they will promise russia thst if they dont sell us anything then they will remove Ukraine conflict related sanction ...Yes, sadly politics is a very big hurdle. If anyone thinks Iran will have a smooth ride for getting Su-30 then they're badly mistaken. Lets assume we go for 100-150 in the long run. This is a change gamer for airforce in the region. Americans, zionists and wahabis will do everything to kill the deal.
What is your problem, ill-tempered friend? I'm merely showing that an attack variant of Yak 130 (e.g. Yak 131/133) nicely fills the bracked now taken up by ancient F-5s (airframes do eventually expire). As for Saegheh, how many produced? How many in service? How many of those are twin seaters? What evidence to support those numbers?What's your point? Your copy pasting info from Wikipedia here to say what exactly?
That Iran's Saegheh is superior to the Yak-130?
Iran's Seagheh is faster, has a higher payload, smaller RCS,... So why on God's green earth would Iran ever purchase the Yak-130 when It can produce a far superior platform?