Procedure to reduce the pressure and temperature on the...

F - Mech Eng,Light,Heat,Weapons – 42 – B

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F42B 10/00 (2006.01) B64C 23/00 (2006.01) F15D 1/10 (2006.01) F42B 10/46 (2006.01) F42B 15/34 (2006.01)

Patent

CA 2325763

A procedure is suggested to reduce pressure and temperature on the front of a missile at ultrasonic speed whereby a spike with a spherical, ellipsoidal, or drop-shaped mount is used on the front end. In contrast to conventional shapes, the sensitive nose of the missile is protected from damaging pressure and temperature, even at high angles of incidence. This makes it possible to create missiles that are highly manoeuvrable at high ultrasonic speeds without high pressures and temperatures arising at the front. The resistance and hence the required thrust of such a missile is strongly reduced when the invention is used which correspondingly increases the range and flight duration of such a missile.

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