Integrated Impulsive Maneuver and Propulsion System Design for Upper Stages Guidance of Spacecrafts, M.Sc. Thesis Sharif University of Technology ; Pourtakdoust, Hossain (Supervisor)
Abstract
This work is an attempt toward an integrated preliminary design of solid rocket (SR) propulsion system for impulsive orbital maneuvers. In this regard a comparative study is initially performed classifying current space propulsion systems and along the goals of this thesis, solid rocket system was selected for our integrated approach. Subsequently, two integration schemes were studied that differed in the primacy of the two design tasks. This study directed our focus to initially size and design an ideal rocket engine and refine it through integration with the maneuver design. Utilizing the ideal rocket concept and its governing equations, a SR was designed to provide the required total...
Cataloging briefIntegrated Impulsive Maneuver and Propulsion System Design for Upper Stages Guidance of Spacecrafts, M.Sc. Thesis Sharif University of Technology ; Pourtakdoust, Hossain (Supervisor)
Abstract
This work is an attempt toward an integrated preliminary design of solid rocket (SR) propulsion system for impulsive orbital maneuvers. In this regard a comparative study is initially performed classifying current space propulsion systems and along the goals of this thesis, solid rocket system was selected for our integrated approach. Subsequently, two integration schemes were studied that differed in the primacy of the two design tasks. This study directed our focus to initially size and design an ideal rocket engine and refine it through integration with the maneuver design. Utilizing the ideal rocket concept and its governing equations, a SR was designed to provide the required total...
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