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The Sparrow emerged from a late-1940s United States Navy program to develop a guided rocket weapon for air-to-air use. In 1947 the Navy contracted Sperry to build a beam-riding version of a standard 5-inch (127 mm) HVAR, the standard unguided aerial rocket, under Project Hotshot. The weapon was initially dubbed KAS-1, then AAM-2, and — from 1948 on — AAM-N-2. The airframe was developed by the Douglas Aircraft Company. The diameter of the HVAR proved to be inadequate for the electronics, leading Douglas to expand the missile's airframe to 8-inch (203 mm) diameter. The prototype weapon began unpowered flight tests in 1947, and made its first aerial interception in 1952.
After a protracted development cycle the initial AAM-N-2 Sparrow entered limited operational service in 1954 with specially modified Douglas F3D Skyknight all-weather carrier night fighters. In 1956, they were joined by the McDonnell F3H-2M Demon and Vought F7U Cutlass fighter aircraft. Compared to the modern versions, the Sparrow I was more streamlined and featured a bullet-shaped airframe with a long pointed nose.
| Category | USAF | USN | Combined |
|---|---|---|---|
| An-2s | — | 2 | 2 |
| MiG-17s | 8 | 5 | 13 |
| MiG-19s | 4 | — | 4 |
| MiG-21s | 38 | 3 | 41 |
| Total | 50 | 10 | 60 |
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The Air Intercept Missile (AIM)-7 Sparrow is a supersonic, medium-range air-to-air missile. The development of this beyond visual range (BVR) missile started as a project called “Hotshot” in 1946 and was intended to design a missile which was capable of intercepting enemy targets at medium range
The AIM-7 Sparrow is a radar-guided, air-to-air missile with a high-explosive warhead
The missile has four major sections: guidance section, warhead, control and rocket motor. It has a cylindrical body with four wings at mid-body and four tail fins.