الصاروخ K-100-1

[النابغة]

تاريخ التصنيع : 1993
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)