Powered part of flight path of unguided rocket influenced by variable cross wind and thrust malalignment is calculated on digital computer; magnitude of deviation caused by distinct disturbances depends on aerodynamic data of missile; optimum yaw oscillation distance decreases with increasing frequency of cross wind.
Influence of aerodynamic parameters on dispersion of unguided rockets due to gusts
AGARD Conference Proc
AGARD Conference ; 1966 Orbits and trajectories
AGARD Conference Proceedings ; n 10
1966
30 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Aeroelasticity as consideration in aerodynamic design of rolling, unguided research rockets
Engineering Index Backfile | 1967
|Aeroballistic optimization of unguided artillery rockets
AIAA | 1978
|