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

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Electromagnetic Systems - 58- Electromagnetic Systems, where a gas is heated in an arc discharge to such a high temperature, that it is converted to neutral plasma (plasma thruster). The plasma is then expelled at high velocity by the interaction of the discharge current with the magnetic field (Lorentz force). A typical application of this principle is the Magneto- Plasma-Dynamic (MPD) type of thruster.
Electrostatic Systems - 59- Electrostatic Systems, where usually a high molecular propellant, such as Xenon gas, is ionized (ion thruster) by e.g. electron bombardment (Kaufman), in a high frequency electromagnetic field (radio-frequency) or by extracting ions from the surface of a liquid metal (cesium) under the effect of a strong electrostatic field (field emission). The ions are then accelerated to high velocity (30 to 60 km/s) by a strong electric field. Electrons are injected into the ion beam from an electron emitter in order to keep it electrically neutral, thus preventing an electric charge build-up of the spacecraft. In addition to the above described category of ion thrusters, the Stationary Plasma Thruster (SPT) which belongs to the category of ‘Hall-effect Thrusters’, uses an applied magnetic field to control electrons in a quasi-neutral plasma discharge.
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- 1- Chapter 1: Introduction to Spa
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S.3 Need of Propulsion Propulsion i
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Orbit control ORBIT CONTROL compris
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S.4 Reaction-Control System - 7- Th
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Solar Sails - 9-
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S.5 Jet Propulsion System - 11- The
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S.6 Spacecraft Propulsion - 13- Spa
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Impulse bits - 15- Impulse bit is t
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Nuclear propulsion Note - 17- SCHEM
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- 1- Chapter 2: Basic Propulsion Eq
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S.3 Basic Equation of Thrust - 3- B
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S.4 Basic Rocket Equation Total Vel
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- 7- S.6 Propulsion Performance Fac
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Test - 9-
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- 11- S.8 Propulsion System Perform
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- 13- S.9 Type of Propulsion System
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Rocket propulsion device basic part
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- 17- The Effective Exhaust Velocit
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Kinetic energy in the expelled mass
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- 1- Chapter 3: Spacecraft Propulsi
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- 3- S.3 Propulsion System Options
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Chemical Propulsion Systems - 5- Ch
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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
Page 69 and 70: Bipropellant Systems (Operate) - 31
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Page 75 and 76: Propellant Tanks - 37-
Page 77 and 78: Unified Propulsion Systems - 39-
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Page 81 and 82: - 43- Main Performance of Bipropell
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Page 85 and 86: Under Development: - 47- A new fami
Page 87 and 88: Solid Propellant Motor - 49-
Page 89 and 90: - 51- Main Performance of Solid Pro
Page 91 and 92: Electric Propulsion Systems - 53- E
Page 93 and 94: Note: - 55- For electric propulsion
Page 95: Power Augmented Catalytic Thruster
Page 99 and 100: - 61- Survey of Electrical Thruster
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Page 103 and 104: Chapter 4: Spacecraft Propulsion Sy
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Page 107 and 108: Important indication - 5 - If we as
Page 109 and 110: S.4 Outline of Advanced Spacecraft
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Page 125: Literature - 23 - Wiley J. Larsson
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S.1 Spacecraft Propulsion Systems Chapter 1: Introduction to ...

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