Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1988-08-05
1990-01-30
Bentley, Stephen C.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
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.
Peretti Claudio
Rebuffatti Guglielmo
A.R.I.S.S.p.A.
Bentley Stephen C.
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