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

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S.9 Summary - 18- Propulsion is needed for launching of spacecrafts, for spacecraft orbit transfer as well as their orbit and attitude control. Here, only propulsion systems will be dealt with which are based on jet propulsion devices that produce thrust by ejecting stored matter, called the propellant. Differences of launch and space propulsion have been mentioned. Propulsion subsystem requirements have been listed. Jet propulsion can be classified according to the source of energy utilized for the ejection of propellant: chemical, electric and nuclear.
- 1- Chapter 2: Basic Propulsion Equations Peter Erichsen, September 2006 S.1 Basic Propulsion Relations This chapter is devoted to the basic laws governing propulsion systems. The chapter will give an overview of the set of equations used in the field of spacecraft propulsion. Understanding these laws is necessary in order to be able to select an appropriate propulsion system and to design its components. The basic laws include the ‘Rocket Equation’, the rocket thrust force and other propulsion performance parameters. In addition two types of propulsion are presented together with the appropriate set of equations characterizing the systems in question.
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 and 16: Impulse bits - 15- Impulse bit is t
Page 17: Nuclear propulsion Note - 17- SCHEM
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
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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-
Page 67 and 68: 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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- 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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