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Aerodynamic characteristics of an ogee-wing space shuttle orbiter concept at a Mach number of 2.01An investigation has been made at a Mach number of 2.01 to determine the effects of a flared rudder on the aerodynamic characteristics of an ogee-wing space-shuttle orbiter configuration. Also investigated were the effects of an upper-aft fuselage fairing for the orbital maneuvering system, elevon deflections, and rudder deflection on the aerodynamic characteristics of the configuration.
Document ID
19720010271
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Putnam, L. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
L-8084
NASA-TM-X-2473
Report Number: L-8084
Report Number: NASA-TM-X-2473
Accession Number
72N17921
Funding Number(s)
PROJECT: RTOP 117-07-01-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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