Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1980-09-05
1983-11-08
Tudor, Harold J.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
137809, 137819, F42B 1502
Patent
active
044137958
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.
REFERENCES:
patent: Re27712 (1973-07-01), Becker et al.
patent: 3135291 (1964-06-01), Kepler et al.
patent: 3212515 (1965-10-01), Zisfein et al.
patent: 3239150 (1966-03-01), Chisel
patent: 3276473 (1966-10-01), Lewis et al.
patent: 3486517 (1969-12-01), Caupa
patent: 3508579 (1970-04-01), Jones
patent: 3521654 (1970-07-01), Brautaset et al.
patent: 3606901 (1971-09-01), Thompson
patent: 3612442 (1971-10-01), Chisel
patent: 3638671 (1972-02-01), Harvey
patent: 3660981 (1972-05-01), Stevens
patent: 3704832 (1972-12-01), Fix et al.
patent: 3717164 (1973-02-01), Griffin
patent: 3752172 (1973-08-01), Cohen et al.
patent: 3797527 (1974-03-01), Bain
patent: 3906979 (1975-09-01), Chapin
patent: 4077572 (1978-03-01), Fitzgerald
"Fluidic Valve for Warm Gas Flow Control", J. T. Kaaselmann, et al, AIAA Paper No. 69-118, Jan. 1969.
"The Vortex Valve Controlled Rocket Motor", C. Nelson, et al, AIAA Paper No. 68-538, Jun. 1968.
"Vortex Valves for Thrust Vector and Jet Interaction Control", Rolf K. Broaderson, et al Guidance and Control.
"A Solid-Propellant Rocket Motor Modulated by a Fluidic Bortex Valve", R. F. Walsh, et al., J. Spacecraft, vol. 8, No. 1, Jan. 1971, pp. 77-79.
"A Vortex Valve for Flow Modulation of 5500.degree. F. Gas", A. Blatter, et al, J. Spacecraft, vol. 7, No. 2, Feb. 1970, pp. 169-174.
McFarland James W.
Miller Albert J.
Miller Leslie S.
The Garrett Corporation
Tudor Harold J.
LandOfFree
Fluidic thruster control and method does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Fluidic thruster control and method, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Fluidic thruster control and method will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-2004449