MISSILE

The invention relates to missiles having an aerodynamic control system, and can be used in guided missiles, interceptor missiles and ballistic missiles. Missile control efficiency is increased by reducing the effect of downwash on the missile, i.e. reversal of the control rolling moment. The present...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: SVETLOV, Vladimir Grigorievich, DORONIN, Viktor Valentinovich, SAMONOV, Viktor Alekseevich, SOKOLOVSKIJ, Viktor Vladimirovich, FILIPPOV, Vladimir Sergeevich, KIRILLOV, Ivan Petrovich
Format: Patent
Sprache:eng ; fre ; rus
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!