NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Mass Uncertainty and Application For Space SystemsExpected development maturity under contract (spec) should correlate with Project/Program Approved MGA Depletion Schedule in Mass Properties Control Plan. If specification NTE, MGA is inclusive of Actual MGA (A5 & A6). If specification is not an NTE Actual MGA (e.g. nominal), then MGA values are reduced by A5 values and A5 is representative of remaining uncertainty. Basic Mass = Engineering Estimate based on design and construction principles with NO embedded margin MGA Mass = Basic Mass * assessed % from approved MGA schedule. Predicted Mass = Basic + MGA. Aggregate MGA % = (Aggregate Predicted - Aggregate Basic) /Aggregate Basic.
Document ID
20130014267
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Beech, Geoffrey
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 27, 2013
Publication Date
May 21, 2013
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
M13-2663
Report Number: M13-2663
Meeting Information
Meeting: 2013 Society of Allied Weight Engineering (SAWE) Annual Meeting
Location: Saint Louis, MO
Country: United States
Start Date: May 21, 2013
End Date: May 22, 2013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available