A buoyant aerial vehicle system includes a balloon, a ballonet configured to selectively receive and discharge a gas to adjust an altitude of the balloon, and an energy regeneration assembly. The energy regeneration assembly includes a turbine and an electric motor. The turbine is coupled to an outlet of the ballonet, such that gas released by the bayonet activates the turbine. The electric motor is operably coupled to the turbine and is configured to convert mechanical energy received from the turbine into electrical energy and convey the electrical energy to a battery.

Balloon altitude control is provided. A system includes a balloon formed from a material having latex. The balloon includes a top portion that is narrower than a middle portion of the balloon. The balloon includes a bottom portion that is in contact with a cable to tether the balloon to a gondola. The bottom portion of the balloon is narrower than the middle portion of the balloon. The system includes a first valve located at the top portion of the balloon. The first valve can open to release gas from within the balloon, and close to at least partially prevent the release of the gas from within the balloon. The system includes a gondola. The gondola includes a control system that can open the first valve to release the gas responsive to a determination to decrease buoyancy of the system.

An altitude control system for an unmanned aerial vehicle includes a compressor assembly defining a plenum therein, a passive valve assembly coupled to a first portion of the compressor assembly and in fluid communication with the plenum, and an active valve assembly coupled to a second portion of the compressor assembly and in fluid communication with the plenum. A method of controlling an altitude of an unmanned aerial vehicle and an unmanned aerial vehicle are also provided.

An altitude control system for an unmanned aerial vehicle includes a compressor assembly defining a plenum therein, a passive valve assembly coupled to a first portion of the compressor assembly and in fluid communication with the plenum, and an active valve assembly coupled to a second portion of the compressor assembly and in fluid communication with the plenum. A method of controlling an altitude of an unmanned aerial vehicle and an unmanned aerial vehicle are also provided.

A lighter-than-air aircraft is provided including a deballasting system, the deballasting system including: at least one tank containing a liquid; a system for pressurizing the liquid of the at least one tank; and at least one sprayer arranged so as to eject the liquid from the pressurization system.

A lighter-than-air aircraft is provided including a deballasting system, the deballasting system including: at least one tank containing a liquid; a system for pressurizing the liquid of the at least one tank; and at least one sprayer arranged so as to eject the liquid from the pressurization system.

A ballast bag that is durable and prevents exposure to FOD is provided. The ballast bag includes a bag body with a first end and a second end, a first side and a second side, and a front side and a rear side. A first strap is connected to the front side forming a loop defined by two parallel lines along the front side of the bag and a handle extending past each end of the bag. A second strap is connected to the rear side forming a loop defined by two parallel lines along the rear side of the bag and a handle extending past each end of the bag. The handles of the straps are the same size to form a double handle on each end of the bag. The first and second strap each have an inner and outer band of embedded non-slip material.

A ballast bag that is durable and prevents exposure to FOD is provided. The ballast bag includes a bag body with a first end and a second end, a first side and a second side, and a front side and a rear side. A first strap is connected to the front side forming a loop defined by two parallel lines along the front side of the bag and a handle extending past each end of the bag. A second strap is connected to the rear side forming a loop defined by two parallel lines along the rear side of the bag and a handle extending past each end of the bag. The handles of the straps are the same size to form a double handle on each end of the bag. The first and second strap each have an inner and outer band of embedded non-slip material.

A ballast dispenser system and method for flight vehicles, such as high altitude lighter than air vehicles. The system passively retains ballast without power and deploys ballast in response to applying power. An electro-permanent magnet passively retains ballast within the dispenser. Application of power to a coil produces an opposing magnetic field that reduces the overall strength of a net magnetic field acting on the ballast. Lateral positional control of the electro-permanent magnet provides calibration and control of the retaining magnetic field strength. A collapsible silo may hold ballast prior to dispensing ballast and collapse upon landing for minimizing damage.

A ballast dispenser system and method for flight vehicles, such as high altitude lighter than air vehicles. The system passively retains ballast without power and deploys ballast in response to applying power. An electro-permanent magnet passively retains ballast within the dispenser. Application of power to a coil produces an opposing magnetic field that reduces the overall strength of a net magnetic field acting on the ballast. Lateral positional control of the electro-permanent magnet provides calibration and control of the retaining magnetic field strength. A collapsible silo may hold ballast prior to dispensing ballast and collapse upon landing for minimizing damage.