AIM-7
Sparrow 
  The AIM-7 Sparrow is a radar-guided, air-to-air missile with a high-explosive warhead.
    The versatile Sparrow has all-weather, all-altitude operational capability and can attack
    high-performance aircraft and missiles from any direction. It is a widely deployed missile
    used by U.S. and NATO (North Atlantic Treaty Organization) forces. 
  
The missile has five major sections: radome, radar guidance system, warhead, flight
    control (autopilot plus hydraulic control system), and solid-propellant rocket motor. It
    has a cylindrical body with four wings at mid-body and four tail fins. Although external
    dimensions of the Sparrow remained relatively unchanged from model to model, the internal
    components of newer missiles represent major improvements with vastly increased
    capabilities. 
  
The AIM-7F joined the Air Force inventory in 1976 as the primary medium-range,
    air-to-air missile for the 
F-15 Eagle. 
  
The AIM-7M, the only current operational version, entered service in 1982. It has
    improved reliability and performance over earlier models at low altitudes and in
    electronic countermeasures environments. It also has a significantly more lethal warhead.
    The latest software version of the AIM-7M is the H-Buildwhich has been produced since 1987
    and incorporates additional improvements in guidance. The 
F-15 Eagle and 
F-16 Fighting Falcon fighters carry the
    AIM-7M Sparrow. U.S. and NATO navies operate a surface-to-air version of this missile
    called the 
RIM-7F/M Sea Sparrow.
  
  
In the Persian Gulf war, the radar-guided AIM-7 Sparrow proved to be a potent air-to-air
    weapon used by Air Force fighter pilots. Twenty-two Iraqi fixed-wing aircraft and three
    Iraqi helicopters were downed by radar-guided AIM-7 Sparrow missiles. 
   
  
    
      | General characteristics | 
    
    
      | Primary function | 
      Air-to-air guided missile  | 
    
    
      | Contractor | 
      Raytheon Co.  | 
    
    
      | Power plant | 
      Hercules MK-58 solid-propellant rocket motor  | 
    
    
      | Thrust | 
      Classified  | 
    
    
      | Speed | 
      Classified  | 
    
    
      | Range | 
      Classified  | 
    
    
      | Length | 
      12 ft | 
      3.64 m  | 
    
    
      | Diameter | 
      8 in | 
      20 cm  | 
    
    
      | Wingspan | 
      3 ft 4 in | 
      1 m  | 
    
    
      | Launch weight | 
      500 lb | 
      227 kg  | 
    
    
      | Guidance system | 
      Raytheon semiactive on either continuous wave
      or pulsed Doppler radar energy  | 
    
    
      | Date deployed | 
      1976  | 
    
    
      | Unit cost | 
      Approximately $125,000  | 
    
    
      | Inventory | 
      Classified  | 
    
  
   
  
  AIM-7 and F-4 Phantom II
  
  Jirka Wagner
  
 
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