S.1 Spacecraft Propulsion Systems Chapter 1: Introduction to ...

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- 16- S.8 Classification of Propulsion Systems Spacecraft propulsion can be classified according to the source of energy utilized for the ejection of propellant: Chemical propulsion use heat energy produced by a chemical reaction to generate gases at high temperature and pressure in a combustion chamber. These hot gases are accelerated through a nozzle and ejected from the system at a high exit velocity to produce thrust force. Electric propulsion uses electric or electromagnetic energy to eject matter at high velocity to produce thrust force. Nuclear propulsion uses energy from a nuclear reactor to heat gases which are then accelerated through a nozzle and ejected from the system at a high exit velocity to produce thrust force.
Nuclear propulsion Note - 17- SCHEMATIC OF A THERMO-NUCLEAR ROCKET ENGINE Turbin Propellant Tank Exhaust Gas Nuclear Reactor Reactor Fuel Element Nozzle Coolant Jacket While chemical and electric systems are used for the propulsion of today’s spacecrafts, nuclear propulsion is still under study. Therefore, only chemical and electric propulsion will be dealt within this book.
Page 1 and 2: - 1- Chapter 1: Introduction to Spa
Page 3 and 4: S.3 Need of Propulsion Propulsion i
Page 5 and 6: Orbit control ORBIT CONTROL compris
Page 7 and 8: S.4 Reaction-Control System - 7- Th
Page 9 and 10: Solar Sails - 9-
Page 11 and 12: S.5 Jet Propulsion System - 11- The
Page 13 and 14: S.6 Spacecraft Propulsion - 13- Spa
Page 15: Impulse bits - 15- Impulse bit is t
Page 19 and 20: - 1- Chapter 2: Basic Propulsion Eq
Page 21 and 22: S.3 Basic Equation of Thrust - 3- B
Page 23 and 24: S.4 Basic Rocket Equation Total Vel
Page 25 and 26: - 7- S.6 Propulsion Performance Fac
Page 27 and 28: Test - 9-
Page 29 and 30: - 11- S.8 Propulsion System Perform
Page 31 and 32: - 13- S.9 Type of Propulsion System
Page 33 and 34: Rocket propulsion device basic part
Page 35 and 36: - 17- The Effective Exhaust Velocit
Page 37 and 38: Kinetic energy in the expelled mass
Page 39 and 40: - 1- Chapter 3: Spacecraft Propulsi
Page 41 and 42: - 3- S.3 Propulsion System Options
Page 43 and 44: Chemical Propulsion Systems - 5- Ch
Page 45 and 46: S.4 Cold and Hot Gas Systems - 7- C
Page 47 and 48: Cold Gas Systems (Operate) - 9- Col
Page 49 and 50: Typical System - 11-
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Page 53 and 54: Advantages Simplicity and reliabili
Page 55 and 56: Liquid Propellants - 17- Characteri
Page 57 and 58: S.6 Liquid Propellant Systems - 19-
Page 59 and 60: Monopropellant Systems (Operate) -
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Page 65 and 66: Diaphragm Tank - 27-
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Advantages Simplicity and reliabili
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Bipropellant Systems (Operate) - 31
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Propellant Tanks - 37-
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Unified Propulsion Systems - 39-
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- 43- Main Performance of Bipropell
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- 45- Dual-Mode systems use hydrazi
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Under Development: - 47- A new fami
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Solid Propellant Motor - 49-
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- 51- Main Performance of Solid Pro
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Electric Propulsion Systems - 53- E
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Note: - 55- For electric propulsion
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Power Augmented Catalytic Thruster
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Electrostatic Systems - 59- Electro
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- 61- Survey of Electrical Thruster
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S.9 Summary - 63- Main characterist
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Chapter 4: Spacecraft Propulsion Sy
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- 3 - S.3 Propulsion System Selecti
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Important indication - 5 - If we as
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S.4 Outline of Advanced Spacecraft
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Exploration of the Solar System - 9
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- 11 - For micro- and nanospacecraf
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wafer 4 wafer 3 wafer 2 wafer 1 Sev
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- 15 - Potential increase in perfor
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- 17 - New Approaches in Advanced P
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- 19 - New Approaches in Advanced P
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- 21 - Exotic Propulsion Methods: A
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Literature - 23 - Wiley J. Larsson
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