Paper shows, by selected examples of experimental French and American missiles, that many aerodynamic problems can lead to failure, if overlooked; most of problems are raised by roll stabilization, by decrease of stability at high Mach numbers, by interaction between propulsive jet and external flow, and by recovery of scientific payloads; it is suggested that specially devised low-density wind-tunnel tests can even help in interpreting some scientific experiments.
Aerodynamic problems of sounding-rocket vehicles
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 5 , n 1
1968
5 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Aerodynamic problems of sounding-rocket vehicles.
AIAA | 1968
|THE AERODYNAMIC PROBLEMS OF THE SOUNDING-ROCKET VEHICLES
AIAA | 1967
|Aeroelastic analysis of sounding rocket vehicles
AIAA | 1973
|