A stored energy release comprises an actuatable member slidably received within a housing. The actuatable member has an extended orientation wherein a portion of the actuatable member extends outwardly from the housing and a retracted orientation wherein the actuatable member resides within the housing. A biasing member is located between the actuatable member and the housing biases the actuatable member to the retracted orientation. A shaft is within the housing with the actuatable member configured for sliding movement along the shaft. A retaining member is located between the actuatable member and the shaft. The retaining member maintains the actuatable member in the extended orientation whereby potential energy is stored within the biasing member. A piezoelectric element selectively engages the retaining member to disable the retaining member and release the stored potential energy within the biasing member to place the actuatable member in the retracted orientation.

A stored energy release comprises an actuatable member slidably received within a housing. The actuatable member has an extended orientation wherein a portion of the actuatable member extends outwardly from the housing and a retracted orientation wherein the actuatable member resides within the housing. A biasing member is located between the actuatable member and the housing biases the actuatable member to the retracted orientation. A shaft is within the housing with the actuatable member configured for sliding movement along the shaft. A retaining member is located between the actuatable member and the shaft. The retaining member maintains the actuatable member in the extended orientation whereby potential energy is stored within the biasing member. A piezoelectric element selectively engages the retaining member to disable the retaining member and release the stored potential energy within the biasing member to place the actuatable member in the retracted orientation.

A device includes a harness system configured to be attached to a parachute harness of a parachute. The device also includes a propulsion system connected to the harness system, wherein the propulsion system is configured to be off when undeployed and during freefall, and wherein the propulsion system is configured to deploy during canopy flight stage to generate thrust for a parachutist of the parachute. The device further includes a circuitry configured to control power generation by the propulsion system to control the thrust. The device includes a power source configured to power the circuitry and the propulsion system.

A harness container for a parachutist has a bio-contoured support cradle or load distributing vest. The load distributing vest, which is generally U-shaped and includes an upper yoke and two straps integral with the yoke, has a multi-layer construction that includes an outer layer and an inner layer mounted on a bio-contoured pad. The outer layer and the inner layer are of corresponding shape and are sewn to one another along a reinforced edging with the pad therebetween. The upper yoke is attached to the front side of the harness container and the ends of the vest straps are attached to the main lift webs so that the vest elevates the harness container and distributes the load thereof across the jumper's shoulders, back and chest for increased comfort.

A harness container for a parachutist has a bio-contoured support cradle or load distributing vest. The load distributing vest, which is generally U-shaped and includes an upper yoke and two straps integral with the yoke, has a multi-layer construction that includes an outer layer and an inner layer mounted on a bio-contoured pad. The outer layer and the inner layer are of corresponding shape and are sewn to one another along a reinforced edging with the pad therebetween. The upper yoke is attached to the front side of the harness container and the ends of the vest straps are attached to the main lift webs so that the vest elevates the harness container and distributes the load thereof across the jumper's shoulders, back and chest for increased comfort.

A powered air vehicle is disclosed. The air vehicle includes a parachute/parafoil or similar lifting body, with a frame structure suspended vertically below the parachute and comprising of all propulsion and flight control systems generally at the upper end of the frame structure. In one embodiment, a propulsion source is mounted on top of the frame structure, which also house the battery module, main parafoil/parachute system, flight control systems, and structure for carrying an individual user below the propulsion source. Control arms control pitch of the propulsion source to control altitude, and are also used to control direction.

A harness container for a parachutist has a bio-contoured support cradle or load distributing vest. The load distributing vest, which is generally U-shaped and includes an upper yoke and two straps integral with the yoke, has a multi-layer construction that includes an outer layer and an inner layer mounted on a bio-contoured pad. The outer layer and the inner layer are of corresponding shape and are sewn to one another along a reinforced edging with the pad therebetween. The upper yoke is attached to the front side of the harness container and the ends of the vest straps are attached to the main lift webs so that the vest elevates the harness container and distributes the load thereof across the jumper's shoulders, back and chest for increased comfort.

A harness container for a parachutist has a bio-contoured support cradle or load distributing vest. The load distributing vest, which is generally U-shaped and includes an upper yoke and two straps integral with the yoke, has a multi-layer construction that includes an outer layer and an inner layer mounted on a bio-contoured pad. The outer layer and the inner layer are of corresponding shape and are sewn to one another along a reinforced edging with the pad therebetween. The upper yoke is attached to the front side of the harness container and the ends of the vest straps are attached to the main lift webs so that the vest elevates the harness container and distributes the load thereof across the jumper's shoulders, back and chest for increased comfort.

A harness container for a parachutist has a bio-contoured support cradle or load distributing vest. The load distributing vest, which is generally U-shaped and includes an upper yoke and two straps integral with the yoke, has a multi-layer construction that includes an outer layer and an inner layer mounted on a bio-contoured pad. The outer layer and the inner layer are of corresponding shape and are sewn to one another along a reinforced edging with the pad therebetween. The upper yoke is attached to the front side of the harness container and the ends of the vest straps are attached to the main lift webs so that the vest elevates the harness container and distributes the load thereof across the jumper's shoulders, back and chest for increased comfort.

A harness container for a parachutist has a bio-contoured support cradle or load distributing vest. The load distributing vest, which is generally U-shaped and includes an upper yoke and two straps integral with the yoke, has a multi-layer construction that includes an outer layer and an inner layer mounted on a bio-contoured pad. The outer layer and the inner layer are of corresponding shape and are sewn to one another along a reinforced edging with the pad therebetween. The upper yoke is attached to the front side of the harness container and the ends of the vest straps are attached to the main lift webs so that the vest elevates the harness container and distributes the load thereof across the jumper's shoulders, back and chest for increased comfort.