NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Project Morpheus: Lessons Learned in Lander Technology DevelopmentNASA'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. Designed, developed, manufactured and operated in-house by engineers at Johnson Space Center, the initial flight test campaign began on-site at JSC less than one year after project start. After two years of testing, including two major upgrade periods, and recovery from a test crash that caused the loss of a vehicle, flight testing will evolve to executing autonomous flights simulating a 500m lunar approach trajectory, hazard avoidance maneuvers, and precision landing, incorporating the Autonomous Landing and Hazard Avoidance (ALHAT) sensor suite. These free-flights are conducted at a simulated planetary landscape built at Kennedy Space Center's Shuttle Landing Facility. The Morpheus Project represents a departure from recent NASA programs and projects that traditionally require longer development lifecycles and testing at remote, dedicated testing facilities. This paper expands on the project perspective that technologies offer promise, but capabilities offer solutions. It documents the integrated testing campaign, the infrastructure and testing facilities, and the technologies being evaluated in this testbed. The paper also describes the fast pace of the project, rapid prototyping, frequent testing, and lessons learned during this departure from the traditional engineering development process at NASA's Johnson Space Center.
Document ID
20140001410
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Olansen, Jon B.
(NASA Johnson Space Center Houston, TX, United States)
Munday, Stephen R.
(NASA Johnson Space Center Houston, TX, United States)
Mitchell, Jennifer D.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
March 13, 2014
Publication Date
September 10, 2013
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-29387
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available