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Aerodynamic characteristics of a family of multistage missiles at a mach number of 6.0

Authors :
Morrisette, E. L
Romeo, D. J
Publication Year :
1965
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1965.

Abstract

Wind tunnel investigation of aerodynamic characteristics of cone-cylinder-flare multistage missile configurations at supersonic speed

Subjects

Subjects :
Aerodynamics

Details

Language :
English
Database :
NASA Technical Reports
Publication Type :
Report
Accession number :
edsnas.19650017042
Document Type :
Report