Fluidic emergency roll control system
Fluidic emergency roll control system
- New search for: Haefner, K. B.
- New search for: Honda, T. S.
- New search for: Haefner, K. B.
- New search for: Honda, T. S.
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.
Document information
Fluidic emergency roll control system
1973-03-01
Report
No indication
English