Author: Richard D. GuhsePublisher:
ISBN:
Category : Injections
Languages : en
Pages : 132
Book Description
Thrust Vector Control by Secondary Injection
Author: Douglas Stacey (University of Manitoba student)Publisher:
ISBN:
Category :
Languages : en
Pages : 68
Book Description
An Investigation of Secondary Injection Thrust Vector Control
Author: Tatsuo YamanakaAn Experimental Investigation of Thrust Vector Control by Secondary Injection
Author: Richard D. GuhsePublisher:
ISBN:
Category : Injections
Languages : en
Pages : 132
Book Description
Secondary Injection Thrust Vector Control
Author: C. A. ZimmermanPublisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
On the basis of experimentally acquired data, thrust vector control systems utilizing secondary injection of fluids into supersonic nozzles have been developed. Several widely divergent theoretical and analytical treatments of the phenomena have appeared as new applications were proposed. The paper reviews the several theories and attempts correlation with the experimental data. Secondary injection thrust vector control results from the injection of fluid (gas or liquid) into the primary exhaust stream of the rocket motor through ports in the divergent section of the nozzle. A shock is induced resulting in a pressure unbalance in the exit cone. The resultant side force, controllable in magnitude and direction, can be utilized for precise vehicle control. (Author).
Proportional Solid Propellant Secondary Injection Thrust Vector Control Study
Author: Two Dimensional Gaseous Secondary Injection Study of Rocket Thrust Vector Control
Author: R. W. MilliganThrust Vector Control Utilizing a Reactive Fluid for Secondary Injection
Author: Donald Arthur PahlPublisher:
ISBN:
Category : Injectors
Languages : en
Pages : 136
Book Description
Rocket Engine Thrust Vector Control Operation Through Secondary Injection by A.B.Billet
Author: A.B. BilletSecondary Injection Thrust Vector Control Utilizing Vortex Amplifiers and Direct Bleed
Author: John G. ClelandPublisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 602
Book Description
Thrust-vector Control by Secondary Injection
Author: FOY JR. MCCULLOUGHPublisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
The technique of thrust-vector control by injection of a fluid into the exhaust stream of a nozzle (secondary injection) was explored. This paper gives a survey of work performed at the Naval Ordnance Test Station during Fiscal Year 1959, previously reported in IDP 765. Both cold-gas (air) data with 3-dimensional and 2dimensional nozzles and data obtained with a liquid-propellant applied-research motor (LPARM) are presented. Fluids studied with the LPARM were N2O4, N2 (gas), H2O, and IRFNA. Physical parameters as well as fluid properties were considered in the tests. Injection of a secondary fluid increases the main thrust of the motor as well as producing a side thrust. Thrust-vector control by secondary injection is simpler and more reliable than mechanical controls and shows promise of becoming a replacement for them. (Author).