Abstract: A system of versatile foundational spacegoing module infrastructure which is a framework of modular hardware and software elements which can be used to rapidly design and produce spacecraft. Preferred embodiments may comprise or include spacecraft modular building elements uniquely suitable for facilitating rapid assembly of numerous custom spacecraft designs from standard modular parts. A craft produced using these elements consists of one of more deltahedral structural frame modules and one or more function modules which provide instrument or subsystem elements. The frame modules provide the spacecraft mechanical structure, power and network distribution. The function modules provide the instruments and subsystems. Combinations of these standard elements can produce an unlimited variety of spacecraft embodiments, as needed for each mission. Supporting technologies may include an androgynous mount interface and a mechanical fastening apparatus for rigid mounting.

Abstract: This is a method and system to lock and release modules on computing devices. The system may include: An automatic lock system for modules on a computing device, the system comprising: a processor connected to a system bus; an input means connected to the processor by the system bus; an output means connected to the processor by the system bus; and a module that inserts into the computing device and is connected to the system bus; a module controller that controls the module and is connected to the system bus; a latch that locks and releases the module to and from the computing device; and a subsystem that controls the latch. The system may also include a basic input/output system (BIOS).