SHOCK SENSING DUAL MODE WARHEAD
Assignee
UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE NAVY. THE
Filed
Aug 27, 1980
Granted
Jan 7, 1997
Location
LA PLATA MD US
Abstract
A shock sensing dual mode warhead is provided for use against both soft andard targets and is capable of sensing which type of target has been struck. The warhead comprises a casing made of a ductile material containing an explosive charge and a fuze assembly. The ductile warhead casing will mushroom upon striking a hard target while still confining the explosive. Proper ductility and confinement are necessary for fuze shock sensing. The fuze assembly contains a pair of parallel firing trains, one initiated only by dynamic pressure caused high impact deceleration and one initiated by low impact deceleration. The firing train actuated by high impact deceleration senses dynamic pressure transmitted, during deformation of the warhead, through the explosive filler which is employed as a fuzing signature. The firing train actuated by low impact deceleration contains a pyrotechnic delay to allow penetration of soft targets.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Feb 17, 1982
Rescinded
Mar 28, 1996
Duration
14 years, 1 month
Inventor
- 1MORLEY C. SHAMBLEN
Record Details
- Patent number
- US 5591935
- Application
- 06186888
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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