Fluidic thruster control and method
US4413795A · kind A · utility
33Cited by
18References
17Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Sep 5, 1980 |
| Grant date | Nov 8, 1983 |
| Priority date | — |
| Expiry date | Sep 5, 2000 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T137/2147
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A fluidic thruster control system and method for guided missiles and the like, which utilizes a fluidic jet interaction device for controlling a downstream fluidic vortex amplifier to modulate exhaust flow through thrust nozzles.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.