A system and method for cleaning a body of a person. The system includes an envelope extending between a top member and a base member, and several rings disposed between the top member and the base member. The envelope, the top member, and the base member define an enclosure of the system. Each ring has several spaced apart nozzles along its circumference and nozzles connect to an air pump. A person can stand on the base member, while the top member can surround the neck of the person. Air under low pressure can then impinge on the body of the person below the neck to remove dirt and dead skin. The dirt and dead skin suspended in the air are drawn through a vacuum source from the inner volume of the enclosure.

A system and method for cleaning a body of a person. The system includes an envelope extending between a top member and a base member, and several rings disposed between the top member and the base member. The envelope, the top member, and the base member define an enclosure of the system. Each ring has several spaced apart nozzles along its circumference and nozzles connect to an air pump. A person can stand on the base member, while the top member can surround the neck of the person. Air under low pressure can then impinge on the body of the person below the neck to remove dirt and dead skin. The dirt and dead skin suspended in the air are drawn through a vacuum source from the inner volume of the enclosure.

An adjustable vehicle seat including a seat frame forming a seat back, the seat frame being configured to couple with an aerospace vehicle, and a seat pan coupled to the seat frame, where one or more of the seat frame and the seat pan is configured to couple the seat pan to the seat frame in one of a plurality of positions relative to the seat frame so that an eye position of a seat occupant relative to instrumentation within the aerospace vehicle is decoupled from a size of the seat occupant.

An adjustable vehicle seat including a seat frame forming a seat back, the seat frame being configured to couple with an aerospace vehicle, and a seat pan coupled to the seat frame, where one or more of the seat frame and the seat pan is configured to couple the seat pan to the seat frame in one of a plurality of positions relative to the seat frame so that an eye position of a seat occupant relative to instrumentation within the aerospace vehicle is decoupled from a size of the seat occupant.

A multifunctional exercise apparatus for exercise of humans, in particular astronauts, said apparatus including a first module comprising a cable reel system operably connected to a torque resistance mechanism, and a second module comprising a flywheel and a brake for providing resistance to the flywheel. The ability provided by the present invention for developing exercises in which the flywheel and a brake in combination with the torque resistance mechanism provides for further possibilities for training body joints and muscle groups.

A multifunctional exercise apparatus for exercise of humans, in particular astronauts, said apparatus including a first module comprising a cable reel system operably connected to a torque resistance mechanism, and a second module comprising a flywheel and a brake for providing resistance to the flywheel. The ability provided by the present invention for developing exercises in which the flywheel and a brake in combination with the torque resistance mechanism provides for further possibilities for training body joints and muscle groups.

Embodiments provide a spacecraft airlock system. Embodiments provide a method and apparatus for attaching space exposed payloads to a space station. The spacecraft airlock system provides a defined volume of space payload to the international space station. The airlock further includes a means of attaching to a space station, a closed structure attached to said means, said means of attaching is capable of robotic manipulation, and a cooling system for cooling payload components within said closed structure.

Examples provide a modular tray table apparatus associated with a console of a seat unit. A tray table carrier unit is removably mounted to a portion of the console. A tray table support element is coupled to the carrier unit and a tray table. The tray table support element movably supports the tray table. A linear displacement mechanism is disposed between the tray table and the tray table support element. The tray table slides along a linear displacement path between a fully retracted configuration and at least one deployed configuration. A rotational displacement mechanism disposed between the tray table and the tray table support element. The tray table slides along a rotational displacement path defined by at least one rotational guide between a linear configuration of the tray table and a substantially perpendicular configuration of the tray table when the tray table is in a fully deployed configuration.

An immobility system for a free-fall environment includes an immobility device including at least one suction cup configured to engage the immobility device to a surface, and a valve that, when activated, results in release of the at least one suction cup from engagement with the surface. A remote controller is spaced apart from the valve and is configured to selectably transmit an activation signal to the valve. An immobility device includes at least one suction cup configured to engage the immobility device to a surface, and a valve that, when activated, results in release of the at least one suction cup from engagement with the surface. A receiver at the device is configured to receive an activation signal and activate the valve.

A supporting frame for aerospace applications comprises a plurality of rods, which are arranged along two bases substantially parallel and opposite each other, and along two sides, which are substantially parallel and opposite to each other and are coupled to each other via the two bases; the rods are coupled to each other in a mutually rotating manner by nodes so as to be able to configure the supporting frame between a deployed operating condition and a compacted operating condition; the nodes are spaced apart from one another in the deployed operating condition and are each hinged to at least two of the rods; in the compacted operating condition, each of the nodes is placed side by side with two adjacent nodes so as to form, together, two supporting members arranged at opposite longitudinal ends of the supporting frame and each being ring-shaped.