41 |
Detonator mechanism |
US30965263 |
1963-09-18 |
US3254602A |
1966-06-07 |
HELMUT KLOSTERMANN; PAUL BEERMANN; RICHARD SCHULTE |
|
42 |
Tear gas gun |
US29849752 |
1952-07-12 |
US2839017A |
1958-06-17 |
SMITH ELMER O |
|
43 |
Signal device |
US45000054 |
1954-08-16 |
US2826144A |
1958-03-11 |
YUKICHI IWATA |
|
44 |
Device to resist the disarming of bombs |
US29158852 |
1952-06-03 |
US2647465A |
1953-08-04 |
JACOB RABINOW |
|
45 |
Manually supported and selfpropelled pulling device |
US67352446 |
1946-05-31 |
US2526714A |
1950-10-24 |
VARNEY FRED M |
|
46 |
All angle of impact inertia fuse |
US72003947 |
1947-01-03 |
US2513536A |
1950-07-04 |
WELLINGTON CARY L |
|
47 |
ANTI-TAMPER DEVICE FOR INTEGRATED CIRCUITS |
PCT/IB2011002331 |
2011-07-15 |
WO2012010971A2 |
2012-01-26 |
FREEDMAN GRAEME JOHN |
An anti-tamper device (10) for one or more integrated circuits (12) includes a firing assembly (14) and a breach assembly (16). The firing assembly (14) includes a contained energy source (24), an impact element (26) and a breach assembly (16). The breach assembly (16) is configured to house one or more integrated circuits (12) and a propeliant charge (30). Upon an attempt to improperly remove or dislodge an integrated circuit (12) from the anti-tamper device (10), the contained energy source (24) is actuated. The energy source (24) propels the impact element (26) against the propeliant charge (30), causing the charge to ignite. The resultant forces from the impact element (26) and ignition of the charge imparts a shock wave through the anti-tamper device (10). This shock wave induces spalling of the integrated circuit (12) such that the circuit is physically altered and rendered unreadable. |
48 |
PENETRATION DETECTION DEVICE |
PCT/US2007015621 |
2007-07-09 |
WO2008108802A3 |
2008-11-20 |
LIPELES JAY; TANENHAUS MARTIN E |
A penetration detection device earned by an earth penetrating bomb includes an inertial measurement unit and a penetrator processor and logic circuit contained in a shock isolated package which can withstand the transmitted environment encountered during earth penetration The inertial measurement unit derives information relative to the attitude of the bomb and the penetrator processor and logic circuit is responsive to the outputs of the inertial measurement unit as well as the outputs of external accelerometers to not only detect the transitions of adjoining layers but count the layers penetrated and also to determine the material of each layer This is compared with a stored layer characterization and if the stored and computed values are in correlation, a signal will be sent to start the arming initiation process A second layer charactepzation may also be stored for comparison if the first layer does not correlate |