Plasma generated between conductive fiber electrodes boosts radar absorption without heavy RAM coatings or nanoparticle dispersion issues.
By calculating aiming points from aircraft attitude and target position, this case reduces UAV pointing errors during pitch and roll maneuvers.
By compensating for roll, pitch, yaw, and angular rates, this case improves aircraft aiming accuracy during maneuvering.
Processor-based pointing logic calculates target position and aircraft orientation to keep airborne aiming accurate during UAV maneuvers.
Separate drone and payload controllers allocate degrees of freedom so heavy active payloads can exert force without degrading hover control.
A rail-and-pin carrier lets air-vehicle weapons be repositioned ergonomically, then locked securely to avoid accidental misdirection.
A low-profile floor brace mounts C4ISR payloads without airframe changes, preserves air drop rails, and supports 360-degree in-flight reconfiguration.
An ambidextrous modular pylon repositions payload carriage to clear weapons bay doors while supporting larger, heavier stores.
A titanium casing with inner insulation and a deflecting protrusion shields helicopter CMDS flare launchers from exhaust heat.
A mode-switching power scheme lets a combat aircraft glide during attack, freeing most onboard electrical power for weapon use.
Multiple magnetic anchoring points and calibrated pins restrain external airborne loads without moving parts, improving reliability under dynamic conditions.
Alternating opposite-side munition release and mechanical interlocks help UAVs stay stable while enabling safe fuse activation and deployment.
Vacuum mounting modules secure missiles to combat drones without pylons, enabling fast field rearming and lower radar reflections.
A coaxial foldable-rotor layout shrinks drone size for covert flight while enabling rapid deployment and ground contact measurements.
A low-profile floor brace transfers payload loads to the aircraft floor, enabling 360-degree sensor view and cargo-compatible reconfiguration.
Removable ammunition trays with latch pins and spring-loaded fittings cut aircraft reloading time while keeping secure attachment in flight.
Bolted floor braces transfer flight loads without airframe changes, preserving cargo rails for air drop operations and payload reconfiguration.
A propellant stream fluidizes powdered fuel from a hopper, reducing reliance on heavy tanks and valves for controlled UAV flame effects.
A servo motor, worm gear, and recoil-disengaging clutch automate gun breech cycling while isolating the drive from firing forces.
A single actuator synchronizes cover opening and ammunition extraction to reduce weight.
This case segments delivery and strike phases, using an attritable STUAS mothership to launch decoys and loitering munitions.
A pyrotechnic release device uses a movable indicator linked to the breech position to verify cartridge presence without opening the chamber.
A rotating frame mechanism orients aerial drone payloads within a hemispherical space below the aircraft body.
Single-axis gimbal mounts weapon through center of gravity to minimize recoil impact, maintaining target alignment and enabling rapid subsequent firing.
A monolithic metallic adaptive member isolates dynamic vibrations while maintaining uniform pressure contact against externally airborne loads.
Active connecting means separate split nosecone halves radially, preventing collision with the missile during slow flight phases.
Elongated support beam spans cabin obstructions via door sill and ceiling attachments, enabling weapon mounting without floor modification.
External fairing mounts payload on aircraft surface to maintain stealth profile while eliminating door panels that cause acoustic and aerodynamic loads.
Deformable monolithic crown panel dissipates bird strike energy, reducing weight and parts count compared to rigid bulkheads.
A pre-stressed ceramic armor plate bonds to a high thermal expansion material, inducing compression stress upon cooling.