Specifications (MiG-27K) Mikoyan MiG-27

file:mig-27

data airforce-technology.com, deagel.com

general characteristics

crew: 1
length: 17.08 m (56 ft)
wingspan:


height: 5 m (16 ft 7 in)
wing area:


empty weight: 11,908 kg (26,253 lb)
loaded weight: 20,300 (44,800 lb)
max. takeoff weight: 20,670 kg (45,570 lb)
powerplant: 1 × khatchaturov r-29-b-300 afterburning turbojet

dry thrust: 78.5 kn (17,650 lbf)
thrust afterburner: 112.8 kn (25,360 lbf)

performance

maximum speed:


range: 2,500 km (1,550 mi; 1,350 nmi)
combat radius: 780 km (480 mi; 420 nmi)


540 km (290 nmi; 340 mi) 2 kh-29 missiles , 3 drop tanks
225 km (120 nmi; 140 mi) 2 kh-29 missiles , no external fuel


ferry range: 2,500 km (1,550 mi; 1,350 nmi)
service ceiling: 14,000 m (46,000 ft)
rate of climb: 200 m/s (39,400 ft/min)
wing loading: 605 kg/m² (123.9 lb/ft²)
thrust/weight: 0.62

armament

guns:


1 × 30 mm gryazev-shipunov gsh-6-30 rotary cannon 260 rounds
1 × 23 mm gryazev-shipunov gsh-23 autocannon 200 rounds


hardpoints: 1 × centerline, 4 × fuselage , 2 × wing glove pylons capacity of 4,000 kg (8,800 lb) and provisions carry combinations of:

rockets:


s-5
s-8
s-25
s-24


missiles:


air-to-air missiles:

r-60m


air-to-surface missiles:

kh-23m
kh-25ml
kh-29l/ml/t/d


anti-radiation missiles:

kh-27ps




bombs:


kab-500kr tv-guided bomb
kab-500l laser-guided bomb
up 500 kg (1,100 lb) bombs








^ [1] mig-27k specs. retrieved 25 january 2015.
^ [2]
^ cite error: named reference frawley_1996 invoked never defined (see page).