Electromagnetic boots for walking in a zero-gravity environment such as in outer space, wherein a pathway made from a magnetic material can be provided. Each boot in includes an electromagnet in a sole of the boot and a control unit configured to magnetize and demagnetize the electromagnet. The control unit can synchronize the pair of electromagnetic boots for walking.

Electromagnetic boots for walking in a zero-gravity environment such as in outer space, wherein a pathway made from a magnetic material can be provided. Each boot in includes an electromagnet in a sole of the boot and a control unit configured to magnetize and demagnetize the electromagnet. The control unit can synchronize the pair of electromagnetic boots for walking.

A spacesuit contaminant removal system includes at least one membrane separator and a liquid sorbent circuit. The at least one membrane separator is configured to receive a spent air stream from a ventilation system of a spacesuit and absorb a contaminant from the spent air stream into a liquid sorbent. The at least one membrane separator is configured to discharge a clean air stream to the ventilation system and discharge the contaminant in a contaminant stream to a space environment using a vacuum of the space environment. The liquid sorbent circuit is configured to circulate the liquid sorbent through the at least one membrane separator.

A spacesuit contaminant removal system includes at least one membrane separator and a liquid sorbent circuit. The at least one membrane separator is configured to receive a spent air stream from a ventilation system of a spacesuit and absorb a contaminant from the spent air stream into a liquid sorbent. The at least one membrane separator is configured to discharge a clean air stream to the ventilation system and discharge the contaminant in a contaminant stream to a space environment using a vacuum of the space environment. The liquid sorbent circuit is configured to circulate the liquid sorbent through the at least one membrane separator.

A magnetic pass-through controller of an in-helmet display includes internal components inside a helmet. The internal components include a magnet assembly holding one or more internal magnets and a swing arm affixed to the magnet assembly and affixed to the in-helmet display. External components outside the helmet include an external magnet housing holding one or more external magnets and an adjuster for manual rotation. The adjuster is coupled to the external magnet housing such that the manual rotation of the adjuster causes a corresponding rotation of the external magnet housing. Magnetic coupling between the one or more internal magnets and the one or more external magnets causes the corresponding rotation also in the magnet assembly and the swing arm.

A magnetic pass-through controller of an in-helmet display includes internal components inside a helmet. The internal components include a magnet assembly holding one or more internal magnets and a swing arm affixed to the magnet assembly and affixed to the in-helmet display. External components outside the helmet include an external magnet housing holding one or more external magnets and an adjuster for manual rotation. The adjuster is coupled to the external magnet housing such that the manual rotation of the adjuster causes a corresponding rotation of the external magnet housing. Magnetic coupling between the one or more internal magnets and the one or more external magnets causes the corresponding rotation also in the magnet assembly and the swing arm.

The disclosure belongs to the field of aerospace technology, and in particular relates to a method of urination and defecation in space. The method may include: forming a sealed space between a spacesuit below the waist and above the two thighs and the human skin before an astronaut urinates or defecates, and using, by the astronauts, the sealed space to urinate or defecate. The disclosure can confine the excrements in a small sealed space, and the operation thereof is simple, convenient and fast, and no excessive cost is required, and no pollution is caused in the spacesuit and the cabin, facilitating the astronauts' work in space.

The disclosure belongs to the field of aerospace technology, and in particular relates to a method of urination and defecation in space. The method may include: forming a sealed space between a spacesuit below the waist and above the two thighs and the human skin before an astronaut urinates or defecates, and using, by the astronauts, the sealed space to urinate or defecate. The disclosure can confine the excrements in a small sealed space, and the operation thereof is simple, convenient and fast, and no excessive cost is required, and no pollution is caused in the spacesuit and the cabin, facilitating the astronauts' work in space.

A system includes a vibration detector to detect a location of vibration and identify a frequency of the vibration. The system also includes a controller to generate audio corresponding to the frequency of vibration detected by the vibration detector and one or more speakers configured to provide the audio as directional sound.

A system includes a vibration detector to detect a location of vibration and identify a frequency of the vibration. The system also includes a controller to generate audio corresponding to the frequency of vibration detected by the vibration detector and one or more speakers configured to provide the audio as directional sound.