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The Tailoring of Traditional Systems Engineering for the Morpheus ProjectNASA's Morpheus Project has developed and tested a prototype planetary lander capable of vertical takeoff and landing that is designed to serve as a testbed for advanced spacecraft technologies. The lander vehicle, propelled by a LOX/Methane engine and sized to carry a 500kg payload to the lunar surface, provides a platform for bringing technologies from the laboratory into an integrated flight system at relatively low cost. From the beginning, one of goals for the Morpheus Project was to streamline agency processes and practices. The Morpheus project accepted a challenge to tailor the traditional NASA systems engineering approach in a way that would be appropriate for a lower cost, rapid prototype engineering effort, but retain the essence of the guiding principles. The team has produced innovative ways to create an infrastructure and approach that would challenge existing systems engineering processes while still enabling successful implementation of the current Morpheus Project. This paper describes the tailored systems engineering approach for the Morpheus project, including the processes, tools, and amount of rigor employed over the project's multiple lifecycles since the project began in FY11. Lessons learned from these trials have the potential to be scaled up and improve efficiency on a larger projects or programs.
Document ID
20140002833
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Devolites, Jennifer L.
(NASA Johnson Space Center Houston, TX, United States)
Hart, Jeremy J.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
April 10, 2014
Publication Date
September 10, 2013
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-29415
Report Number: JSC-CN-29415
Funding Number(s)
PROJECT: Morpheus Project 743588.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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