NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
Reliability Estimation for Mission Extension NASA Approach/RecommendationsPresent NASA's current and recommended concepts for Mission Extension and De-orbit reliability Methodologies. NASA's current and recommended approaches ensuring de-orbit requirements are not unnecessarily driving mission design efforts or adding incresed costs or risks to manufacturing solutions without providing benefit to missionsand will assist in moving reliability estimation from piece part performance estimates to component history and system-level testing based estimations.
Document ID
20190025797
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
DiVenti, Tony (NASA Headquarters Washington, DC United States)
Leitner, Jesse (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Lindsey, Nancy (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Petrick, Dave (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Evans, John (NASA Headquarters Washington, DC United States)
Date Acquired
June 9, 2019
Publication Date
June 6, 2019
Subject Category
Astronautics (General)
Report/Patent Number
GSFC-E-DAA-TN68926
Report Number: GSFC-E-DAA-TN68926
Meeting Information
Meeting: SMA Trilateral Working Group Meeting
Location: Darmstadt
Country: Germany
Start Date: June 6, 2019
End Date: June 7, 2019
Sponsors: European Space Agency, NASA Headquarters
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
SMA
Mission Extension
Post-Mission Disposal
Reliability

Related Records

There are no records associated with this record.
No Preview Available