Air supported structure equipment particularly suitable for ball

Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control

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Details

244120, 102384, F42B 15033

Patent

active

048968455

ABSTRACT:
Air carrying equipment particularly suited for ballistic type munitions, consisting of two parts that can be mutually coupled: a saddle that can be mounted to straddle the munition, provided with a pair of wings that are opposite and hinged close to the longitudinal edges of the saddle; and a cradle that can be mounted underneath the body of the munition, which can be coupled to saddle and contains fuel tanks, a motor device in the rear and an ogival part or torpedo nose in front with air intake and wind rotor.

REFERENCES:
patent: 1448166 (1923-03-01), Strong
patent: 2314942 (1943-03-01), Hinchcliff
patent: 2423090 (1947-07-01), Fink et al.
patent: 4447025 (1984-05-01), Bock et al.

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