Gas jet steering device and method missile comprising such a device
US4463921A · kind A · utility
39Cited by
6References
12Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Apr 20, 1982 |
| Grant date | Aug 7, 1984 |
| Priority date | — |
| Expiry date | Apr 20, 2002 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF42B10/663
- WIPO fieldOther special machines
- WIPO sectorMechanical engineering
Abstract
A steering device comprising an annular element having N exhaust nozzles and a rotary element disposed coaxially inside said annular element; the rotary element comprising M gas passageways may be positioned in MN discrete directions so as to provide a transverse thrust force orientated in one of the steering planes.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.