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
A fuselage/tank structure study for actively cooled hypersonic cruise vehicles: Aircraft design evaluationThe effects of fuselage cross sections and structural members on the performance of hypersonic cruise aircraft are evaluated. Representative fuselage/tank area structure was analyzed for strength, stability, fatigue and fracture mechanics. Various thermodynamic and structural tradeoffs were conducted to refine the conceptual designs with the primary objective of minimizing weight and maximizing aircraft range.
Document ID
19750018925
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nobe, T. (McDonnell Aircraft Co. Saint Louis, MO, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-132668
Report Number: NASA-CR-132668
Accession Number
75N26997
Funding Number(s)
CONTRACT_GRANT: NAS1-12995
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

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