Abstract: A system and method interface one or more secondary payloads to a launch vehicle. A Multiple Interface Payload Subsystem (MIPS) is configured with one or more circuit boards to provide a secondary payload interface for each of the one or more secondary payloads. The MIPS couples with the launch vehicle using a single launch vehicle interface that provides communication and power from avionics of the launch vehicle. Each of the secondary payloads couples to one of the secondary payload interfaces. The MIPS provides communication and power from the launch vehicle to each of the secondary payloads via the single launch vehicle interface and a respective one of the secondary payload interfaces.

Abstract: Systems and methods reduce development, integration and testing time of a spacecraft implemented with one or more reconfigurable processor boards. Mission spacecraft design tools design, configure, simulate and analyze the spacecraft based upon constraints of the mission requirements. The mission spacecraft design tools utilize a database of defined module specifications and firmware components. One or more RPBs are programmed based upon the configuration and interfaced to other end item components defined by the configuration to form the spacecraft.