초록 ▼

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

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.

대표청구항 ▼

[ What is claimed is:] [1.] A rocket comprising lattice control surfaces, the rocket comprising a propulsion system located in a body (1), an apparatus of control and guidance systems, fixed wings (2) and lattice control surfaces (3) of a control system, located on a body (1) in regular intervals ar

[ What is claimed is:] [1.] A rocket comprising lattice control surfaces, the rocket comprising a propulsion system located in a body (1), an apparatus of control and guidance systems, fixed wings (2) and lattice control surfaces (3) of a control system, located on a body (1) in regular intervals around a centerline of the body and having lifting surfaces formed by planes (9), characterized in that the wings (2), lattice control surfaces (3) of the control system and the body (1) are made in such a manner that they have the following dimension ratios: ]EQU3 ] [6.] A lattice control surface of a rocket, comprising a load-carrying frame of a rectangular shape, including side bars (18, 19), root (22) and tip (23) planes and units adapted for attachment of the lattice control surface (3) to a drive shaft, and a set of planes (24, 25) of different thickness located inside a frame, forming a lattice as honeycomb, characterized in that side bars (18, 19) of the frame are made with smoothly decreasing thickness, the root (22) and tip (23) planes of the frame made of different thickness; and planes (24, 25) of a lattice are made with smooth or discrete reduction of thickness, narrowing at length of a plane from root to tip portion along the span of a control surface.