تويت
الطول : 7.4 م
القطر : 510 ملم
طول الجناح : 75 سم
الوزن الاطلاق: 750 كلغ
السرعة : 4 ماخ
المدى : 400 كلم !
التوجيه: راداري نشط
 Mockup of KS–172 in front of Su-30 in 1994 |
|
| Long range air-to-air missile | |
| Russia & India | |
| NPO Novator & DRDO | |
| 748 kg (1,650 lb) (KS–172)[1] | |
| 6.01 m (19.7 ft) + 1.4 m (4.6 ft) (KS–172)[1] | |
| 40 cm (16 in) (KS–172)[1] | |
| HE fragmentation (KS–172)[1] | |
| 50 kg (110 lb) | |
| Solid-propellant tandem rocket booster (KS–172)[1] | |
| 61 cm (24 in) (KS–172)[1] | |
| At least 200 km,[2] possibly 300–400 km (160–210 nmi) | |
| 3 m (9.8 ft)–30,000 m (98,000 ft) (KS–172)[1] | |
| 4,000 km/h (2,500 mph; 1.1 km/s; Mach 3.3) (KS–172)[1] | |
| inertial navigation with midcourse guidance and terminal active radar homing (KS–172)[1] | |
| Su-27, Su-30, Su-35,[3] Su-30MKI[1] PAK FA (expected) |
|