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Free-flight investigation of longitudinal stability and control of a rocket-propelled missile model having cruciform, triangular, inline wings and tails
Author:
Hall, James R
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L51J17
Link:
https://digital.library.unt.edu/ark:/67531/metadc59083/
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