Guided missile with at least one engine for producing forward thrust
US11768062B2 · kind B2 · utility
0Cited by
6References
20Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Jan 14, 2022 |
| Grant date | Sep 26, 2023 |
| Priority date | — |
| Expiry date | Jan 14, 2042 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C2009/005
- WIPO fieldOther special machines
- WIPO sectorMechanical engineering
Abstract
A guided missile with a sleeve-shaped missile body, at least one engine for producing forward thrust, at least one flight direction control device, and at least one aerodynamic extension. The least one flight direction control device is rotatably mounted to a top area and/or a bottom area of the sleeve-shaped missile body for adjusting a flight direction of the guided missile. The least one aerodynamic extension comprises an aerodynamic cross-sectional shape that is arranged on a left-hand side and/or a right-hand side of the sleeve-shaped missile body.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.