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ROCKET THRUST CONTROL BY GAS INJECTION.

ROCKET THRUST CONTROL BY GAS INJECTION. PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 87

Book Description


ROCKET THRUST CONTROL BY GAS INJECTION.

ROCKET THRUST CONTROL BY GAS INJECTION. PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 87

Book Description


Rocket Thrust Vector Control by Secondary Gas Injection

Rocket Thrust Vector Control by Secondary Gas Injection PDF Author: C. K. Lee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

Book Description


Performance of Small (100-lb Thrust) Rockets Motors Using Coaxial Injection of Hydrazine and Nitrogen Tetroxide

Performance of Small (100-lb Thrust) Rockets Motors Using Coaxial Injection of Hydrazine and Nitrogen Tetroxide PDF Author: Joseph F. Wasserbauer
Publisher:
ISBN:
Category : Propulsion systems
Languages : en
Pages : 32

Book Description


Secondary Injection for Solid Rocket Thrust Magnitude Control

Secondary Injection for Solid Rocket Thrust Magnitude Control PDF Author: Richard Eugene Gardner
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

Book Description


Vortex Flow and Erosion in Rocket Nozzles Due to Warm-gas Injection for Thrust Vector Control

Vortex Flow and Erosion in Rocket Nozzles Due to Warm-gas Injection for Thrust Vector Control PDF Author: G. Louis Smith
Publisher:
ISBN:
Category : Gas
Languages : en
Pages : 36

Book Description


A STUDY OF ROCKET THRUST CONTROL BY GAS INJECTION.

A STUDY OF ROCKET THRUST CONTROL BY GAS INJECTION. PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 123

Book Description
A theoretical and experimental investigation of thrust control by secondary gas injection was completed. Thrust control is treated from the two aspects of thrust modulation and vector control. The thrust modulation study is concerned with the use of injection as a means of throttling the main nozzle flow. The performance (flow throttling and thrust) of a variety of secondary injection configurations was measured with a low pressure-ratio, axially symmetric nozzle as well as a high pressure-ratio, two-dimensional nozzle. The flow throttling results agree with an anlysis based on three flow models and the schlieren photographs (from the two-dimensional tests) show that all three types of flow occur. The vector control study concerns asymmetric secondary gas injection as a means of controlling the direction of the thrust vector.

Analysis of Injection-velocity Effects on Rocket Motor Dynamics and Stability

Analysis of Injection-velocity Effects on Rocket Motor Dynamics and Stability PDF Author: Herbert G. Hurrell
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

Book Description


Two Dimensional Gaseous Secondary Injection Study of Rocket Thrust Vector Control

Two Dimensional Gaseous Secondary Injection Study of Rocket Thrust Vector Control PDF Author: R. W. Milligan
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

Book Description


An Attempted Experimental Investigation of Rocket Thrust Vector Control by Secondary Liquid Injection

An Attempted Experimental Investigation of Rocket Thrust Vector Control by Secondary Liquid Injection PDF Author: Philip Alan Graham
Publisher:
ISBN:
Category :
Languages : en
Pages : 110

Book Description


Thrust Vector Control Requirement for Launch Vehicles Using a 260-inch Solid Rocket First Stage

Thrust Vector Control Requirement for Launch Vehicles Using a 260-inch Solid Rocket First Stage PDF Author: Carl J. Daniele
Publisher:
ISBN:
Category :
Languages : en
Pages : 72

Book Description