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Configuration evaluation and criteria plan. Volume 1: System trades study and design methodology plan (preliminary). Space Transportation Main Engine (STME) configuration studyThe System Trades Study and Design Methodology Plan is used to conduct trade studies to define the combination of Space Shuttle Main Engine features that will optimize candidate engine configurations. This is accomplished by using vehicle sensitivities and engine parametric data to establish engine chamber pressure and area ratio design points for candidate engine configurations. Engineering analyses are to be conducted to refine and optimize the candidate configurations at their design points. The optimized engine data and characteristics are then evaluated and compared against other candidates being considered. The Evaluation Criteria Plan is then used to compare and rank the optimized engine configurations on the basis of cost.
Document ID
19870009171
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bair, E. K.
(Aerojet Technical Systems Co. Sacramento, CA, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1986
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
DR-9-VOL-1
NASA-CR-178939
RPT/BB0324-VOL-1
NAS 1.26:178939
Report Number: DR-9-VOL-1
Report Number: NASA-CR-178939
Report Number: RPT/BB0324-VOL-1
Report Number: NAS 1.26:178939
Accession Number
87N18604
Funding Number(s)
CONTRACT_GRANT: NAS8-36867
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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