Abstract: A bolometer pixel trigger array includes a substrate, an electrically conductive contact pad formed on the substrate, and bolometer formed on the substrate. The bolometer includes at least one thermally conductive trigger arm having a fixed end coupled to a portion of the bolometer and an electrically conductive free end configured to deflect with respect to the fixed end. At least one trigger arm establishes different operating states of the bolometer pixel trigger in response to the at least one trigger arm realizing different temperatures. The different operating states are configured to change an electrical connection between the at least one trigger arm and the contact pad.

Abstract: A bolometer pixel trigger array includes a substrate, an electrically conductive contact pad formed on the substrate, and bolometer formed on the substrate. The bolometer includes at least one thermally conductive trigger arm having a fixed end coupled to a portion of the bolometer and an electrically conductive free end configured to deflect with respect to the fixed end. At least one trigger arm establishes different operating states of the bolometer pixel trigger in response to the at least one trigger arm realizing different temperatures. The different operating states are configured to change an electrical connection between the at least one trigger arm and the contact pad.

Abstract: A high speed radio frequency signal interconnect device provides for signal communication within a system at cryogenic temperatures. The device includes a plurality of conductive traces provided on a first dielectric substrate where the ends of the traces have a predetermined shape. A second dielectric substrate covers the first dielectric substrate leaving the ends of the traces exposed. A connector is coupled to each respective end and includes pins coupled to a respective trace. Each connector is configured to define a respective isolating chamber about each of the first ends of the conductive traces where the pins are attached.

Abstract: A launch canister for a missile, including an outer canister shell and a concentric inner liner. The inner liner augments the canister shell with structural load capability and bending inertia to enhance canister stiffness. The inner liner can be constructed from structural load carrying composite materials, and also acts as a thermal and ablative insulator to enable vertical plume venting away from the enveloped missile. A shock and vibration isolation layer can be laminated between the inner liner and canister shell.

Abstract: A launch canister for a missile, including an outer canister shell and a concentric inner liner. The inner liner augments the canister shell with structural load capability and bending inertia to enhance canister stiffness. The inner liner can be constructed from structural load carrying composite materials, and also acts as a thermal and ablative insulator to enable vertical plume venting away from the enveloped missile.