The Syrian airfield prepare for reception of military aircraft of China
The latest news about fast emergence in borders of Syria of navy of China encouraged Syrians and res[...]
ІУІШ-21ЦІУІ / 7///BB
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The MiG-21UM and MiG-21US differed mainly in their instrumentation |
Specifications
Span, 7.154 ш (23 ft 5.7 in); fuselage length (except cone and probe),
12.18 m (39 ft 11.5 in); wheel track, 2.692 m (8 ft 10 in); wheel base,
4.806 m (15 ft 9.2 in); wing area, 23 m2 (247.6 sq ft); takeoff weight, 8,000 kg (17,630 lb); fuel, 2,030 kg (4,475 lb); wing loading, 347.8 kg/m2 (71.3 lb/sq ft); max operating limit load factor, 7.
Performance
Max speed, 2,175 km/h at 13,000 m (1,175 kt at 42,640 ft); max speed at sea level, 1,150 km/h (621 kt); climb rate at sea level in clean configuration, 150 m/sec (29,530 ft/min); climb to 16,800 m (55,100 ft) in 8 min; service ceiling, 17,300 m (56,745 ft); landing speed, 250-260 km/h (135-140 kt); range, 1,210 km at 14,000 m (750 mi at 47,920 ft), with 800-1 (211-US gal) drop tank, 1,460 km (905 mi); takeoff roll, 900 m (2,950 ft); landing roll with SPS and tail chute, 550 m (1,800 ft).