A method for configuring an interior of a reconfigurable vehicle using one or more cabin modules. The method comprises providing, by a user interface system, a plurality of possible cabin configuration options to a plurality of users for selection by the plurality of users so as to generate selection data indicative of cabin configuration options selected by the users. The cabin configuration options relate to types of configuration of the one or more cabin modules. The method comprises determining an availability of cabin configuration options based on inventory data which relates to types of configuration of cabin modules that are currently available for use so as to generate availability data, and generating a forecast of cabin modules predicted to be loaded on the reconfigurable vehicle based on the selection data and the availability data. The method further comprises updating the availability data and the selection data substantially in real time based on the inventory data and user input to the user interface system so as to generate updated availability data and updated selection data, and modifying the forecast based on the updated availability data and the updated selection data. The method comprises finalizing the forecast so as to generate commissioning data indicative of cabin modules to be loaded on the reconfigurable vehicle, loading the reconfigurable vehicle with one or more cabin modules based on the commissioning data, and updating the inventory data based on the cabin modules that are loaded on the reconfigurable vehicle.

Methods, systems, and apparatuses are disclosed for conditioning or blending light for increasing the uniformity of light distribution and light wavelength customization, and light arrays integrated into structural and non-structural assemblies and sub-assemblies in cabin interiors.

Methods, systems, and apparatuses are disclosed for conditioning or blending light for increasing the uniformity of light distribution and light wavelength customization, and light arrays integrated into structural and non-structural assemblies and sub-assemblies in cabin interiors.

Methods, systems, and apparatuses are disclosed for conditioning or blending light for increasing the uniformity of light distribution and light wavelength customization, and light arrays integrated into structural and non-structural assemblies and sub-assemblies in cabin interiors.

Methods, systems, and apparatuses are disclosed for conditioning or blending light for increasing the uniformity of light distribution and light wavelength customization, and light arrays integrated into structural and non-structural assemblies and sub-assemblies in cabin interiors.

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.

A conformal seat insert for an adjustable vehicle seat, the conformal seat insert comprising an insert frame, the insert frame having one or more insert reference features for locating the insert frame on a seat frame of the vehicle seat in a predetermined position relative to the seat frame, and a contoured support surface formed in the insert frame, the contoured support surface having a crew reference point corresponding to an acromial point of a shoulder of a seat occupant of the adjustable vehicle seat, the crew reference point being a datum from which an eye position of the seat occupant is established relative to instrumentation of an aerospace vehicle in which the adjustable vehicle seat is located.

A conformal seat insert for an adjustable vehicle seat, the conformal seat insert comprising an insert frame, the insert frame having one or more insert reference features for locating the insert frame on a seat frame of the vehicle seat in a predetermined position relative to the seat frame, and a contoured support surface formed in the insert frame, the contoured support surface having a crew reference point corresponding to an acromial point of a shoulder of a seat occupant of the adjustable vehicle seat, the crew reference point being a datum from which an eye position of the seat occupant is established relative to instrumentation of an aerospace vehicle in which the adjustable vehicle seat is located.

A method of the producing artificial gravity in an electromagnetized environment is provided with a bodysuit, a corridor, a plurality of mobile electromagnets, a plurality of mobile inertial measurement units (IMUs), a plurality of first fixed electromagnets, second fixed electromagnets, and at least one computing unit. The first fixed magnets and the second fixed magnets are integrated throughout the corridor to continuously generate a uniform magnetic field through the corridor. The mobile electromagnets are integrated throughout the bodysuit to electromagnetically interact with the first fixed electromagnets and the second fixed electromagnets, which simulates gravity as the bodysuit moves through the corridor. The mobile IMUs are integrated to the bodysuit so that the mobile IMUs sends spatial positioning and orientation data to the computing unit. This feedback data allows for better gravity simulation because the computing unit can then directionally and magnitudinally adjust the electromagnetic field of each mobile electromagnet.

Embodiments provide a spacecraft airlock system. Embodiments provide a method and apparatus for attaching space exposed payloads to a space station.