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

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The curves m PS /m S/C 1,0 0,8 0,6 0,4 0,2 0,0 - 4 - ∆v-Performance Range of Built Spacecraft Propulsion System Concepts (Examples) I =193 Ns/kg ssp (Nitrogen) Cold Gas I ssp =654 Ns/kg (Ammonia) I ssp =1440 Ns/kg Hydrazine Bipropellant SPT Electric Propulsion Systems 500 1000 1500 2000 2500 3000 I ssp =1862 Ns/kg I ssp =2354 Ns/kg I ssp =2746 Ns/kg I ssp =6375 Ns/kg I ssp =10 801 Ns/kg delta-v (m/s)
Important indication - 5 - If we assume mPS/mS/C< 0.30, we can read directly from the curves of mPS/mS/C: For low ∆v
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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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S.4 Cold and Hot Gas Systems - 7- C
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Cold Gas Systems (Operate) - 9- Col
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Typical System - 11-
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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
Page 83 and 84: - 45- Dual-Mode systems use hydrazi
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 and 96: Power Augmented Catalytic Thruster
Page 97 and 98: Electrostatic Systems - 59- Electro
Page 99 and 100: - 61- Survey of Electrical Thruster
Page 101 and 102: S.9 Summary - 63- Main characterist
Page 103 and 104: Chapter 4: Spacecraft Propulsion Sy
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Page 109 and 110: S.4 Outline of Advanced Spacecraft
Page 111 and 112: Exploration of the Solar System - 9
Page 113 and 114: - 11 - For micro- and nanospacecraf
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Page 117 and 118: - 15 - Potential increase in perfor
Page 119 and 120: - 17 - New Approaches in Advanced P
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Page 123 and 124: - 21 - Exotic Propulsion Methods: A
Page 125: Literature - 23 - Wiley J. Larsson
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S.1 Spacecraft Propulsion Systems Chapter 1: Introduction to ...

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