A missile container sealing assembly uses a linkage assembly to pivot doors open via the projectile's forward motion.
An electric circuit heats a fixing device to break it, releasing a compressed spring that launches a parachute without complex mechanical parts.
A separable stealth shell encases aircraft effectors to minimize radar backscatter cross-section.
Eccentric bearing units rotate and translate a rotary door inward, eliminating external airflow exposure that causes drag and noise during operation.
A missile launcher tube uses a lever system to open and close the barrel without dedicated motors.
A rocket launcher aiming device uses a pivotable raising lever to reposition the elevation axis for compact transport.
An inductive weapon interface system transfers power and data wirelessly, reducing qualification time by enabling universal module integration.
A weapon station rail integrates inductive power couplers to transfer energy wirelessly between the platform and loaded munition.
A modular weapon system uses a segmented barrel and releasable locking device to configure propellant charges and countermass for optimal recoilless performance.
Distributed gas injection in a ram accelerator launches multiple payloads, reducing G-loads and operational expenses.
A kinematic linkage pivots a missile canister from storage to launch position.
A compact umbilical cable disconnect device uses a spacer component to maintain separation between the cutter and cable prior to severance.
A radial launcher array rotates continuously to deliver countermeasures against ballistic threats.
A modular interface apparatus uses rocket motors to propel a missile from a launch platform.
Elastic blades with intermediate sliding means enable complete reclosure of missile containers, preventing gas penetration under high pressure.
A radar absorbent material tow line accelerates a cruise missile in flight to start its engine.
A multi-mission munition adapter integrates missile launchers and bomb ejectors onto a single aircraft hardpoint.
Modular launch containers on a rotatable base resolve the trade-off between structural stability and reloading flexibility.
Merged propulsion and separation functions eliminate complex PADs, reducing weight and impulsive shock.
A gas generator uses a pusher plate to impart initial velocity to projectiles via controlled gas flow.
Real-time processing extracts statistical parameters from raw measurements, reducing memory capacity and energy consumption for long-term missile storage.
A motorized firing arm rotates pyrotechnic devices to generate arcuate visual effects, resolving the limited range of stationary gerb displays.
Nested non-axisymmetric boosters around a central booster reduce projectile weight while increasing propellant volume and egress control.
Vertical launch tubes rotate to provide full azimuth coverage while minimizing radar cross-section and deck space usage.
Elastic deformation of the tab stop allows controlled axial translation, resolving manual assembly bottlenecks.
Calibrated arming apparatus with flexible drop links prevents shear wire jamming by maintaining equal tension and angle on the fuze unit.
A segmented launcher housing isolates sensitive munition sensors from exhaust plumes during transport and launch.
A UAV weapon adapter isolates firearm recoil forces through a dedicated mounting assembly, enabling stable flight for small unmanned aerial vehicles.
A weapon assembly microcontroller stores barrel bore axis deviation data to compensate for alignment errors without mechanical adjustment.
A movable flap transitions to a withdrawn position to minimize hydrodynamic swirl and noise generation.
A sliding keeper manages cable slack within a torpedo tube guide channel to prevent snagging during loading and unloading operations.
Outwardly flaring tabs on a heat-treated ABS clip friction-fit into umbilical slot grooves, preventing cable chafing and degradation during installation.
A floatable housing rises to the surface to deploy unmanned aerial vehicles, resolving detectability risks during rapid launch operations.
Autonomous UAV sonar buoys deploy via rocket launch to reach predetermined coordinates, replacing inefficient manned vessel operations.
A weapon nozzle uses a circumferential element to minimize forward recoil without requiring a liquid countermass.
A variable diameter nozzle adjusts its cross-sectional area to vent gases during slow cook off, preventing housing rupture while preserving thrust generation.
A modular weapon carriage system uses vertical translation and locking mechanisms to support airborne stores.
A holding device uses a snap-action catch to secure the pin during projectile launch.
A modular weapon platform uses a rocker arm on a rotor to elevate missiles and projectile weapons for independent aiming.
A passive shutter uses two flexible panels to seal a launch tube opening automatically.
A marine rocket erection device uses a guide member to constrain sliding motion and drive the assembly.
Autonomous vessel deploys unmanned combat aerial vehicles to create a protective defense cloud around critical assets.
A submarine payload ejection system uses a cable to transmit piston force through a sealed aperture.
Arcuate rail member minimizes actuator forces and reduces installation space while maintaining high positioning accuracy.
Hydraulic water injection into the hull offsets mass loss from deployed munitions, preventing listing and maintaining maneuverability.
Spiral guide arms engage stabilizing fins to extract wrongly loaded mortar shells, eliminating manual tilting risks.
Segmented connector savers absorb blast effects to protect reusable launcher connectors, reducing reloading times and preserving guidance reliability.
A hermetic covering system protects moisture-sensitive projectile components using a dedicated bag and desiccant layer.
Nested telescoping piston springs provide controlled separation force without debris or extreme shock loads.
A smart translator box bridges analog and digital interfaces without hardware modifications.