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
Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a Mach number of 2.01Lateral and longitudinal aerodynamic characteristics of hypersonic missile configurations with canard controls in supersonic pressure tunnel
Document ID
19670022204
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Foster, G. V. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1959
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-134
Report Number: NASA-TM-X-134
Accession Number
67N31533
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC VEHICLE
LONGITUDINAL STABILITY AND CONTROL
PRESSURE TUBE
LATERAL STABILITY AND CONTROL
AERODYNAMIC CHARACTERISTICS
CANARD

Related Records

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