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

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Orbit Maintenance or “Station Keeping”: - 6- - Keeping a spacecraft in the desired mission orbit, i.e. compensating for effects of disturbing forces like drag, solar wind, gravitational forces, etc. Attitude control Changing the attitude, that is changing the orientation of a spacecraft to the desired direction. Keeping a spacecraft to the desired direction by compensating for disturbing torques.
S.4 Reaction-Control System - 7- There are the following types of reaction control systems: Reaction Jets (propulsion): which produce a control force by the expenditure of mass; Solar Sails, Magnetic Torquers (magnetic coils): which produce a control force by interaction with the environmental field; Momentum-Transfer Devices (reaction-, flywheels): which produce no net control force, but simply transfer angular momentum to or from the spacecraft. Odin Satellite Swedish small satellite project for astronomical and atmospheric research. Launched in February 2001 on a Start-1 launch vehicle from Svobodny.
Page 1 and 2: - 1- Chapter 1: Introduction to Spa
Page 3 and 4: S.3 Need of Propulsion Propulsion i
Page 5: Orbit control ORBIT CONTROL compris
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 and 16: Impulse bits - 15- Impulse bit is t
Page 17 and 18: Nuclear propulsion Note - 17- SCHEM
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
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S.6 Liquid Propellant Systems - 19-
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Monopropellant Systems (Operate) -
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- 23-
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- 25-
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Diaphragm Tank - 27-
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Advantages Simplicity and reliabili
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Bipropellant Systems (Operate) - 31
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- 33-
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- 35-
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Propellant Tanks - 37-
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Unified Propulsion Systems - 39-
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- 41-
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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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