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Nuclear Engine System Simulation (NESS). Version 2.0: Program user's guideThis Program User's Guide discusses the Nuclear Thermal Propulsion (NTP) engine system design features and capabilities modeled in the Nuclear Engine System Simulation (NESS): Version 2.0 program (referred to as NESS throughout the remainder of this document), as well as its operation. NESS was upgraded to include many new modeling capabilities not available in the original version delivered to NASA LeRC in Dec. 1991, NESS's new features include the following: (1) an improved input format; (2) an advanced solid-core NERVA-type reactor system model (ENABLER 2); (3) a bleed-cycle engine system option; (4) an axial-turbopump design option; (5) an automated pump-out turbopump assembly sizing option; (6) an off-design gas generator engine cycle design option; (7) updated hydrogen properties; (8) an improved output format; and (9) personal computer operation capability. Sample design cases are presented in the user's guide that demonstrate many of the new features associated with this upgraded version of NESS, as well as design modeling features associated with the original version of NESS.
Document ID
19930014686
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Pelaccio, Dennis G.
(Science Applications International Corp. Torrance, CA., United States)
Scheil, Christine M.
(Science Applications International Corp. Torrance, CA., United States)
Petrosky, Lyman
(Science Applications International Corp. Torrance, CA., United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1993
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-191081
E-7623
NAS 1.26:191081
Report Number: NASA-CR-191081
Report Number: E-7623
Report Number: NAS 1.26:191081
Accession Number
93N23875
Funding Number(s)
CONTRACT_GRANT: NAS3-25809
PROJECT: RTOP 593-71-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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