Enhanced payload delivery
A device may include a set of payloads and a mechanism. The set of payloads may be configured to interact with at least one of an airborne device or a component of the airborne device via at least one of physical entanglement, sensor obscuration, or surface adhesion. The mechanism may be operable between an inactive state and an active state. The mechanism may be configured to transition to the active state in response to inductive energy generated by relative motion through a magnetic field during launch, and deploy the set of payloads based on at least one of one or more elapsed times during travel of the device along the trajectory, one or more positions of the device along the trajectory, or one or more distances traveled by the device along the trajectory.
1 . A device configured to travel along a trajectory, the device comprising:
a set of payloads configured to interact with at least one of an airborne device or a component of the airborne device via at least one of physical entanglement, sensor obscuration, or surface adhesion; and
a mechanism operable between an inactive state and an active state,
wherein the mechanism is configured to:
transition to the active state in response to inductive energy generated by relative motion through a magnetic field during launch, and
deploy the set of payloads based on at least one of:
one or more elapsed times during travel of the device along the trajectory,
one or more positions of the device along the trajectory, or
one or more distances traveled by the device along the trajectory,
wherein at least one payload of the set of payloads includes a set of visual cues including at least one of the physical entanglement, a tracer compound, a color-coded dye, or a phosphorescent marker, the set of visual cues being configured to indicate at least one of a release path or an interaction region.
2 . The device of claim 1 , wherein at least one of the physical entanglement, the sensor obscuration, or the surface adhesion comprises:
physically entangling using an entanglement element,
providing contact-based disruption using at least one fragment,
impairing at least one sensor using airborne obscurant particles,
providing thermal interference,
providing spectral sensing disruption, or
providing adhesive surface alteration.
3 . The device of claim 1 , wherein at least one payload comprises particles having shapes and sizes configured to promote suspension in air and impair at least one sensor associated with the airborne device, the shapes comprising at least one of a flake shape or a spherical shape and the sizes being less than or equal to 100 microns.
4 . The device of claim 1 , wherein at least one payload comprises an entanglement element composed of at least one of an ultra-high-molecular-weight polyethylene (UHMWPE), a nylon, a polyester, a cellulose, or a cellulose-based material, and
wherein the entanglement element is configured to at least one of unwind or unravel during travel of the device along the trajectory to create an entanglement volume.
5 . The device of claim 1 , wherein the mechanism, to deploy the set of payloads, is further configured to utilize at least one of:
a spring-loaded deployment system,
a pyrotechnic actuator,
an inertially-triggered release system activated by at least one of an acceleration threshold or a velocity threshold, or
a rupture-based pressure vessel configured to fail along a pre-weakened seam associated with the device.
6 . The device of claim 1 , wherein at least one payload comprises a set of particles including at least one of magnetically-responsive materials or iron-containing particles configured to impair at least one of a magnetic system or an electronic system of the airborne device.
7 . The device of claim 1 , wherein the set of payloads includes one or more entanglement elements coupled to the device and configured to be deployed, during travel of the device along the trajectory, in a direction opposite to a direction of travel of the device, the one or more entanglement elements further being configured to at least one of unroll or extend to form an elongated aerial denial volume,
wherein the device is stabilized based on the one or more entanglement elements.
8 . The device of claim 1 , wherein the physical entanglement includes one or more streamers.
9 . The device of claim 1 , wherein the physical entanglement includes one or more filaments.
10 . A device configured to travel along a trajectory, the device comprising:
a set of payloads configured to interact with at least one of an airborne device or a component of the airborne device via at least one of physical entanglement, sensor obscuration, or surface adhesion; and
a mechanism operable between an inactive state and an active state,
wherein the mechanism is configured to:
transition to the active state in response to inductive energy generated by relative motion through a magnetic field during launch, and
deploy the set of payloads based on at least one of:
one or more elapsed times during travel of the device along the trajectory,
one or more positions of the device along the trajectory, or
one or more distances traveled by the device along the trajectory,
wherein at least one payload includes at least one of a set of fluids or a set of gels including at least one of a glycerin-based mist, a biodegradable tackifier, a cyanoacrylate-based, a urethane material, a latex material, or a rubber-based agent configured to provide adhesive surface alteration.
11 . A system, comprising:
a first device comprising:
a set of payloads configured to interact with at least one of an airborne device or a component of the airborne device via at least one of physical entanglement, sensor obscuration, or surface adhesion;
a mechanism operable to transition from an inactive state to an active state; and
a second device configured to create a magnetic field and impart motion to the first device, the first device being configured to travel along a trajectory based on the motion,
wherein the mechanism is configured to:
transition to the active state based on inductive energy generated by moving through the magnetic field, and
deploy the set of payloads based on at least one of:
one or more elapsed times during travel of the first device along the trajectory,
one or more positions of the first device along the trajectory, or
one or more distances traveled by the first device along the trajectory,
wherein the mechanism is further configured to deploy payloads sequentially to form multiple interaction zones, and
wherein interaction zones, of the multiple interaction zones, are at least one of spatially distinct from one another or formed at different times.
12 . The system of claim 11 , wherein the first device comprises a housing configured to separate, during travel of the first device along the trajectory, into one or more fragments that disperse in air, the one or more fragments being configured to physically engage with at least one of the airborne device or the component of the airborne device.