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Military


Su-24 FENCER (SUKHOI)

Specifications
Country of Origin CIS (formerly USSR)
Similar Aircraft
  • Tornado
  • F-111
  • F-14 Tomcat
  • F-15 Eagle
  • MiG-23/-27 Flogger
Crew Two
Role
  • all-weather attack
  • fighter-bomber
  • strike
Length 69 ft, 6 in (20 m)
Span 56 ft, 6 in (17.26 m)
Ceiling 16500 meters
Cruise range 1930nm
In-Flight Refueling Yes
Internal Fuel 10385 kg
Payload 8000 kg
Armament
  • cannon
  • missiles
  • bombs
Guns Onboard 23mm gun with 500 rds
Guided air-to-surface missiles
  • Kh-25ML
  • Kh-25MR (Kh-23M)
  • Kh-29L
  • Kh-29T
  • Kh-58E,
  • Kh-58E-01 (lit. A, A', B, C)
  • Kh-31P (lit. A, A', B, B', C)
  • Kh-31A
  • Kh-59,
  • Kh-59ME
  • S-25LD
    • Guided air-to-air missiles
  • R-60MK (R-60),
  • R-73E
    • Guided bomb units
  • KAB-500KR,
  • KAB-500L
    • Air bombs
  • AB-100
  • AB-250 (M54)
  • AB-250 (M62)
  • AB-500M-54
  • ODAB-500PM
    • Cluster bombs
  • RBK-250
  • RBK-500
    • Incendiary bombs S-24B
    Unguided missiles S-25-OFM
    Small-size cargo pods KMGU-2
    Pod guns SPPU-6
    External fuel tanks
  • PTB-2,000 (1,860 l)
  • PTB-3,000 (3,050 l)
    • Suspension points 8
    Sensors Fencer radar, terrain-following radar, LRMTS, RWR, Advanced bombsight
    Drop Tanks 3000 L drop tank with 2396kg of fuel for 233nm range
    Armament Cannon: GSh-6N-30 30mm rotary
    AS-7/9/10/11/12/14, AA-8, FAB-500, TN-1000, AA-11
    User Countries
    • Azerbaijan
    • Belarus
    • CIS
    • Iran
    • Kazakhstan
    • Libya
    • Syria
    • Ukraine

    Su-24M Specifications

    :
    Crew 2 people
    Length 24.594 m (with LDPE)
    scope of the wing at an angle of sweep = 16 ° 17,638 m
    at an angle of sweep = 69 ° 10,366 m
    Height 6.193 m
    Wing area at an angle of sweep = 16 °: 55,16 m²
    at an angle of sweep = 69 °: 51 m²
    Elongation of the wing at an angle of sweep = 16 °: 5,64
    at an angle of sweep = 69 °: 2,107
    Sweep angle on the leading edge 16 ° / 35 ° / 45 ° / 69 °
    V-wing cross -4,5 °
    The base chassis 8.51 m
    Track Chassis 3.31 m
    Weight empty 22,300 kg
    Curb weight 23,700 kg
    Normal takeoff weight 33,500 kg
    Maximum takeoff weight 39,700 kg
    Normal landing weight 24,500 kg
    Maximum landing weight 28,000 kg
    weight of fuel in internal tanks 9800 kg
    volume of fuel tank 11860 l
    Powerplant 2 × turbofan AL-21F-G - 2 × 7800 kg (76.5 to H)
    Afterburner thrust 2 × 11,200 kg (110 kN)
    Flight characteristics
    Maximum speed at an altitude of 200 meters 1320 km / h (without pods) at a high altitude of 1600 km / h (M = 1.35)
    Take-Off speed 360-400 km / h
    Landing speed 285-310 km / h
    Combat radius 560 kilometers (at an altitude of 200 meters with PTB and normal combat load)
    Ferry range 2850 km (with PTB)
    Service ceiling 11,500 m
    Wing loading 607 kg / m² (at normal take-off weight at = 16 °)
    Thrust-to-weight ratio 0.67 / 0.56 (normal / maximum take-off weight in afterburner)
    Takeoff run 1150-1250 m (in normal takeoff weight)
    Landing length 950-1000 m (in normal takeoff weight and a drag parachute)
    Maximum operating overload + 6,5G
    Weaponry
    Gunnery 1 x six-barreled 23-mm cannon GSH-6-23 500 fn.
    The combat load 7500 kg (maximum), 8 suspension points
    Guided Missiles rocket "air-to-air"
  • 2 × R-60 (AA-8)

    missiles "air-land":
  • 4 × Kh-25ML / MR or X-23
  • 3 × X 29L / T or X-59
  • 6 × S-25L
  • 2 × X 58
    • Unguided rockets
  • 192 (32 × 6) × 57 mm P-5 in blocks 32 or UB-
  • 120 (20 × 6) × 80 mm C-8 in blocks B-8M or
  • 30 (6 × 5) × 122 mm C-13 in blocks B-13L or
  • 4 × 240 mm C-24 or
  • 6 × 266 mm C-25
    • Bombs
  • 3 × 1500 kg (FAB-1500, KAB-1500L / TC, and so on. D.) Or
  • 7 × 500 kg (KAB-500L / KR, ST-500) or
  • 10 × 500 kg (FAB-500, RBC 500) or
  • 16 × 30 or 250 kg (FAB-250, RBC 250) or
  • 38 × 100 kg (OFAB-100) or
  • 7 × 2 containers KMGU
    • Cannon containers 3 × SPPU-6 with 23 mm cannon GSH-6-23 with 400 rounds

    Su-24MK Specifications

    :
    Aircraft performance
    Takeoff weight:
         - normal, kg 38,040
         - maximum, kg 43,755
    Maximum landing weight, kg 27,900
    Maximum internal fuel, kg 11,100
    Normal ordnance load, kg 3,000
    Maximum ordnance load, kg 8,000
    Service ceiling (without external ordnance and stores), km 11
    Maximum flight speed at sea level (without external ordnance and stores), km/h 1,315
    Max Mach (without external ordnance and stores) 1.35
    G-limit (operational) 6
    Operational radius of action at sea level in mixed mode (Vcr in the 200-km area, V=900 km/h in other areas) with PTB external fuel tanks and 6x FAB -500M-62 bombs, km 615
    Ferry flight range with 2xPTB-3000 external fuel tanks, km:
         - with PTB external fuel tanks dropped 2,775
         - with one in-flight refuelling 5,000
    Takeoff run at normal take-off weight, m 1,550
    Landing run at normal landing weight (with braking parachute), m 1,100
    Aeroplane dimensions:
         - length, m 24.532
         - wingspan, m 17.638 (10.366)
         - height, m 6.193
    Crew 2
    In-flight refuelling system
    Maximum flow rate (at entry pressure of 3.5 kg/cm 2), l/min 1,100
    Powerplant
    Number and type of engines 2 x AL-21FZA
    Thrust:
         - in afterburner, kgf 111,200
         - at full power, kgf 11,200
    Avionics
         1. Attack and navigation system
              1.1. Digital computer device
              1.2. Doppler navigator
              1.3. Optical sighting device
              1.4. I/O device (I/O)
              1.5. On-board switchgear (OBS)
              1.6. Photo recording equipment set
              1.7. Control signal conditioner
              1.8. Onboard module of Tekon-1 television guidance system
              1.9. Laser/TV search and track system (LTVSTS)
              1.10. Radio command linkage
              1.11. Passive radar:
         - letter A and A' instrumentation pod
        - letter B, B' and C instrumentation pod
              1.12. Nose radar scanner (NRS)
              1.13. Collision-warning radar (CWR)
              1.14. Small-size inertial instrument system
              1.15. Low-range radio altimeter
              1.16. NRS video signal onboard processing block
              1.17. TV display
              1.18. GPS satellite-based navigation system
         2. Autopilot system
         3. IFF equipment
         4. VHF-UHF communications transceiver
         5. Short-wave radio
         6. Automatic direction finder
         7. Aircraft responder
         8. Electronic countermeasures system
              8.1. Radar warning receiver
              8.2. Jamming capabilities control device
              8.3. Active jamming system
              8.4. Infrared search and track sensor (IRSTS)
              8.5. Cartridge ejection mechanism
         9. Integrated defensive aids suite
         10. Long-range radiotechnical navigation system
         11. Short-range radiotechnical navigation system
         12. Flight data recorder system
         13. Camera
         14. Tape-recording mechanism, solid-state storage unit
         15. Combat performance monitoring equipment
         16. VCR
         17. Weapons control system

    * As per equipment delivery specification

    Armaments
    1. Guns Onboard 23mm gun with 500 rds
    2. Guided air-to-surface missiles Kh-25ML
    Kh-25MR (Kh-23M)
    Kh-29L
    Kh-29T
    Kh-58E,
    Kh-58E-01 (lit. A, A', B, C)
    Kh-31P (lit. A, A', B, B', C)
    Kh-31A
    Kh-59,
    Kh-59ME
    S-25LD
    3. Guided air-to-air missiles R-60MK (R-60), R-73E
    4. Guided bomb units KAB-500KR, KAB-500L
    5. Air bombs: AB-100
    AB-250 (M54)
    AB-250 (M62)
    AB-500M-54
    ODAB-500PM
    6. Cluster bombs RBK-250
    RBK-500
    7. Incendiary bombs S-24B
    8. Unguided missiles: S-25-OFM
    9. Small-size cargo pods KMGU-2
    10. Pod guns SPPU-6
    11. External fuel tanks PTB-2,000 (1,860 l),
    PTB-3,000 (3,050 l)
    12. Suspension points 8



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