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AA.10

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AKA: Project 5101. Status: Operational 1950. Thrust: 1.96 kN (441 lbf).

Starting point was the German X4. During development solid propellant adopted in lieu of liquid propellants, two stages in place of one. Tests in 1950-1951 from a Ju.88 aircraft were successful, and the missile was developed further into the AA.20.