Rocket Propulsion Elements

@inproceedings{Sutton1963RocketPE,
  title={Rocket Propulsion Elements},
  author={George P. Sutton and Howard S. Seifert},
  year={1963},
  url={https://api.semanticscholar.org/CorpusID:122781135}
}
Classification definitions and fundamentals nozzle theory and thermodynamic relations flight performance chemical rocket propellant performance analysis liquid propellant rocket engine fundamentals liquid propellants thrust chambers combustion of liquid propellants turbopumps, engine design, engine controls, calibration, integration and optimization solid propellant rocket fundamentals solid propellants combustion of solid propellants solid rocket components and motor design hybrid propellant… 

Solid Propellant Rocket Motors

Liquid Rocket Propellants Past And Present Influences And

Internal Combustion Processes of Liquid Rocket EnginesRocket PropulsionInvestigation of Liquid Rocket PropellantsBaseline Computational Fluid Dynamics Methodology for Longitudinal-Mode

Solid Propellant Rockets

Propulsion theoretical and experimental analysis of composite propellants motors

Rockets have revolutionized space technology and human space exploration. Most rockets and missiles are both propelled by rocket motors that use composite solid propellants. The ICT code and the NSAS

Fundamental Concepts on Liquid-Propellant Rocket Engines

The engine of a rocket vehicle is a machine which produces thrust by accelerating a gas flowing through the machine. The reaction to this acceleration is the force which drives the vehicle. The

Analysis of the Rocket Plug Nozzle Combined Cycle Propulsion System

Preliminary analysis of a new type of Rocket Based Combined Cycle Propulsion System is presented using analytical and computational methods combined with experimental data to predict plume interaction characteristics.

Conceptual design and performancenumerical modeling of hybrid propulsion motor

Conceptual design algorithm of hybrid rocket motor with solid fuel and liquid oxidizer is investigated in this study. Hybrid chemical rocket propulsion is presently of interest due to reduced system

Performance Evaluation of Hybrid Propellant Rocket Engine

In this article, the potential of the hybrid propellant rocket engine technique is discussed. it is a great dream to flight engineers to design and fabricate a rocket engine with more reliability and

Nozzle Optimization of Dual Thrust Rocket Motors

Optimizing the nozzle of a solid propellant rocket motor plays an essential rule in the overall performance of the motor. In this paper, the investigation of an optimization model of dual thrust

Numerical Analysis of Regenerative Cooling in Liquid Propellant Rocket Engines for Ground Testing

    N. Oo
    Engineering, Physics
  • 2018
In liquid propellant rocket engine must be required cooling techniques for high combustion temperature during long operation. In this study propellants of liquid rocket engine for ground testing are
...