Abstract: An apparatus for development and/or testing of a payload for a satellite, comprising: a payload interface operable to connect to the payload; and a communication link, operable to couple the apparatus with a computer; wherein the apparatus is operable to emulate one or more subsystems of the satellite, such that the behaviour of the payload when connected to the apparatus via the payload interface and communication link is the same as when in the satellite.
Type:
Application
Filed:
March 7, 2017
Publication date:
March 28, 2019
Applicant:
Open Cosmos Ltd.
Inventors:
Rafael Jordá SIQUIER, Han LAI, Aleix Megias HOMAR, Jordi Barrera ARS, Mark COWAN