Rocket with lattice control surfaces

The group of inventions pertains to rocket technology, in particular guided rockets, and can be used in various types and classes of rocket with lattice control surfaces, and in the rocket control surfaces. The rocket is of a standard aerodynamic design and comprises a body (1) with a motor assembly...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	VLADIMIR NOKOLAEVICH BELYAEV, GENNADY ALEXANDROVICH SOKOLOVSKY, VLADIMIR GRIGORIEVICH BOGATSKY
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AMMUNITION AVIATION BLASTING COSMONAUTICS EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	The group of inventions pertains to rocket technology, in particular guided rockets, and can be used in various types and classes of rocket with lattice control surfaces, and in the rocket control surfaces. The rocket is of a standard aerodynamic design and comprises a body (1) with a motor assembly, a guidance and control system apparatus, fixed wings (2) and movable lattice control surfaces (3) of a control system, said control surfaces being spaced evenly on the outer body along the latter's longitudinal axis. In the reinforcement frame, side members (18, 19) are designed so as to narrow towards the end region of the control surface; the root surface (22) is broader than the end surface (23), the thickness of the lattice planes (24, 25) narrowing either continuously or in steps towards the end region.