DocumentCode :
1886243
Title :
Morpheus lander testing campaign
Author :
Hart, Jeremy J. ; Mitchell, Jennifer D.
Author_Institution :
Johnson Space Center, NASA, Houston, TX, USA
fYear :
2012
fDate :
3-10 March 2012
Firstpage :
1
Lastpage :
12
Abstract :
NASA´s Morpheus Project has developed and tested a prototype planetary lander capable of vertical takeoff and landing designed to serve as a testbed for advanced spacecraft technologies. The Morpheus vehicle has successfully performed a set of integrated vehicle test flights including hot-fire and tether tests, which will ultimately culminate in an un-tethered “free-flight”. This development and testing campaign was conducted on-site at the Johnson Space Center (JSC), less than one year after project start. Designed, developed, manufactured and operated in-house by engineers at JSC, the Morpheus Project represents an unprecedented departure from recent NASA programs and projects that traditionally require longer development lifecycles and testing at remote, dedicated testing facilities. This paper documents the integrated testing campaign, including descriptions of test types (hot-fire, tether, and free-flight), test objectives, and the infrastructure of JSC testing facilities. A major focus of the paper will be the fast pace of the project, rapid prototyping, frequent testing, and lessons learned from this departure from the traditional engineering development process at NASA´s Johnson Space Center.
Keywords :
aerospace testing; space vehicles; Morpheus Project; Morpheus lander testing campaign; NASA; free-flight test; frequent testing; hot-fire test; integrated testing campaign; planetary lander; rapid prototyping; spacecraft technology; tether test; vertical takeoff and landing; Ignition; NASA; Propulsion; Software; Testing; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2012 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4577-0556-4
Type :
conf
DOI :
10.1109/AERO.2012.6187304
Filename :
6187304
Link To Document :
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