Loading...
Please wait, while we are loading the content...
Similar Documents
Fluidic emergency roll control system. [for emergency aircraft control following failure of primary roll control system
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Honda, T. S. Haefner, K. B. |
| Copyright Year | 1973 |
| Description | A fluidic emergency roll control system for aircraft stabilization in the event of primary flight control failure was evaluated. The fluidic roll control units were designed to provide roll torque proportional to an electrical command as operated by two diametrically opposed thrust nozzles located in the wing tips. The control package consists of a solid propellant gas generator, two diametrically opposed vortex valve modulated thrust nozzles, and an electromagnetic torque motor. The procedures for the design, development, and performance testing of the system are described. |
| File Size | 6022363 |
| Page Count | 96 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740001936 |
| Archival Resource Key | ark:/13960/t4wh7bj60 |
| Language | English |
| Publisher Date | 1973-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Nozzle Design Performance Tests Gas Generators Nozzle Flow Aircraft Equipment Systems Analysis Lateral Control Aircraft Control Fluidic Circuits Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
