Low thrust chemical rocket technology
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Low thrust chemical rocket technology by Steven J. Schneider

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Published by National Aeronautics and Space Administration, For sale by the National Technical Information Service in [Washington, DC, Springfield, Va .
Written in English

Subjects:

  • Rockets (Aeronautics),
  • Space vehicles -- Propulsion systems.

Book details:

Edition Notes

StatementSteven J. Schneider.
SeriesNASA technical memorandum -- 105927., NASA technical memorandum -- 105927.
ContributionsUnited States. National Aeronautics and Space Administration.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL14687793M

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Low thrust chemical rocket technology An on-going technology program to improve the performance of low thrust chemical rockets for spacecraft on-board propulsion applications is reviewed. Improved performance and lifetime is sought by the development of new predictive tools to understand the combustion and flow physics, introduction of high temperature materials and improved component .   Liquid Fuels / Liquid Monopropellants / Gaseous Propellants / Safety and Environmental Concerns / Problems / References / 8 Thrust Chambers Injectors / Combustion Chamber and Nozzle / Low-Thrust Rocket Thrust Chambers or Thrusters / Chemical Rocket Thrust Specific Impulse Rocket equation Efficiency Trajectories High-exhaust-velocity, low-thrust trajectories Plasma and electric propulsion Fusion propulsion Basics A rocket engine is an engine that produces a force, (a thrust) by creating a high velocity output without using any of the constituents of the "atmosphere" in. The book then elaborates on rocket flight trajectory, basic principles of stabilization and steering, and ground equipment and launching devices. The publication is a valuable source of information for engineers and researchers interested in rocket technology.

Low-Thrust Rocket Thrust Chambers or Thrusters Materials and Fabrication Heat Transfer Analysis General Steady-State Heat Transfer Relations Transient Heat Transfer Analysis Steady-State Transfer to Liquids in Cooling Jacket Radiation Starting and Ignition Useful Life of Thrust Price: $ THE DEFINITIVE INTRODUCTION TO ROCKET PROPULSION THEORY AND APPLICATIONS The recent upsurge in global government and private spending and in space flight events has resulted in many novel applications of rocket propulsion technology. Rocket Propulsion Elements remains the definitive guide to the field, providing a comprehensive introduction to essential concepts and .   Solar drive provides low thrust as compared to the very high thrust of a chemical rocket. This is a good thing, for the fragile plastic bubble will tolerate only low accelerations. It will be necessary to remain under power for hours to achieve the acceleration obtained in minutes by a chemical power plant. The thrust equation which describes the basic relations of a chemical rocket was first given in by the Russian Konstantin Tsiolkovskiy. Assuming a fricti onless, 1-D flow of an ideal gas with.