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Military


AA-10 ALAMO R-27

Specifications
Contractor Vympel
NidekR-27P1 R-27EP1
Date Deployed1982
Range
  • 2 - 80 km R-27R 
  • 70 km R-27T 
  • 130 km R-27RE 
  • 120 km R-27TE
  • 72110
    Target destruction altitude, km0.02 - 20
    SpeedMach 4
    PropulsionOne solid-propellant rocket motor
    Guidance
  • SARH  R-27R, R-27E 
  • All-aspect Infrared  R-27T, R-27TE
  • Warhead39 kg expanding rod
    Launch Weight
  • 253 kg R-27R 
  • 254 kg R-27T 
  • 350 kg R-27RE 
  • 343 kg R-27TE
  • 248346
    Length3.70 m4,0474.742
    Diameter230 mm
    body diameter: solid rocket motor 0.230.26
    Fin Span0.77 m 0.7740.803
    scope of the rudders 0.972
    Platforms
  • Su-27
  • Su-33
  • Su-35
  • Mig-29
  • Yak-141





  • 0.23
    Specifications
    Modification:R-27R1R-27ER1R-27T1R-27ET1R-27P1R-27EP1
    Weight, kg:253350245343248346
    Length, m:4.14.83.84.54.04.7
    Diameter (caliber), m:
    Engine diameter, m:0.230.260.230.260.230.26
    Wingspan, m:0.770.80.770.80.770.8
    Rudder range, m:0.97
    Launch height, km:to 25until the 27thto 25until the 27thto 20
    Maximum launch range, km:
    in PNS:6093508478110
    in the SNS:18261520
    Maximum overload, g:85
    Weight of the warhead, kg39
    Guidance system:ON RL GSN with correctionPassive IR GOSPassive RL GSN



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