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

Recommendations

Info

Comparison - 62- THRUSTER COMPARISON: Typical Electrical vs. Chemical Figures (Data listed are indicative only)
S.9 Summary - 63- Main characteristics of candidate spacecraft propulsion systems; Classification of propulsion systems listed based on type of energy source; Basic configurations of propulsion systems explained; Main performance characteristics of propulsion systems listed; Advantages and disadvantages of propulsion systems discussed; Still to be done: Propulsion system performances to be evaluated with regard to mission impulse and velocity-increment requirements in order to enable you to select and size propulsion systems. This will be done in the next chapter.
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 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-
Page 51 and 52: - 13-
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) -
Page 61 and 62: - 23-
Page 63 and 64: - 25-
Page 65 and 66: Diaphragm Tank - 27-
Page 67 and 68: Advantages Simplicity and reliabili
Page 69 and 70: Bipropellant Systems (Operate) - 31
Page 71 and 72: - 33-
Page 73 and 74: - 35-
Page 75 and 76: Propellant Tanks - 37-
Page 77 and 78: Unified Propulsion Systems - 39-
Page 79 and 80: - 41-
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: - 61- Survey of Electrical Thruster
Page 103 and 104: Chapter 4: Spacecraft Propulsion Sy
Page 105 and 106: - 3 - S.3 Propulsion System Selecti
Page 107 and 108: Important indication - 5 - If we as
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
Page 115 and 116: wafer 4 wafer 3 wafer 2 wafer 1 Sev
Page 117 and 118: - 15 - Potential increase in perfor
Page 119 and 120: - 17 - New Approaches in Advanced P
Page 121 and 122: - 19 - New Approaches in Advanced P
Page 123 and 124: - 21 - Exotic Propulsion Methods: A
Page 125: Literature - 23 - Wiley J. Larsson
show all

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

Create successful ePaper yourself

Delete template?

Save as template?