Abstract
The Air Force Research Laboratory (AFRL) developed an initial plug-and-play (PnP) capability for spacecraft, similar to USB on personal computers, which better defines hardware and software interfaces and incorporates self-discovery and auto-configuration in order to simplify spacecraft development and reduce cost and schedule. PnP technology was matured through a suborbital PnP flight experiment in September 2007 and a secondary Spacecraft Avionics Experiment (SAE) payload on the TacSat-3 satellite, which launched in May 2009. AFRL developed and submitted a complete set of PnP standards through the American Institute of Aeronautics and Astronautics (AIAA) in 2011. Space electronics to adapt existing satellite components and implement full PnP on satellites in accordance with these AFRL standards was independently developed in alternate hardware implementations by Goodrich Corp under AFRL and by Northrop Grumman under Operationally Responsive Space (ORS). In 2011, AFRL conducted a cost-benefit analysis of PnP and assembled a collaborative review board (CRB) in Sept 2011 to evaluate PnP. This CRB was comprised of representatives from Space and Missiles Center (SMC), National Reconnaissance Organization (NRO), Naval Research Laboratory (NRL), John Hopkins University (JHU) Applied Physics Laboratory (APL), The Aerospace Corporation, and several large commercial and DOD satellite developers. This CRB laid out a transition path to develop and implement PnP standards for implementation in large (>1000 kg) DOD and commercial satellites. Transition of PnP technology into operational systems continues in PnP architecture studies for SMC, PnP products from multiple space industry vendors, commercial implementations of PnP, and the Northrop Grumman ORS-2 spacecraft currently project to fly in 2014–2015. This paper provides details related to development of PnP technology, AFRL's cost-benefit analysis of PnP, recommendations of the PnP CRB, and on-going efforts to mature and fly PnP technology.
Published Version
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