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

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S.5 Summary - 22 - Selection process involves a variety of propulsion options, such as systems operated with cold gas, liquid monopropellant and bipropellant, or some form of electric propulsion. Primarily, propulsion systems have to meet mission impulse and velocity increment ∆v requirements. Therefore, the evaluation of propulsion system performances is a primary task in the selection process. The ‘System specific Impulse’, Issp, allows a more accurate determination of the propulsive performance of spacecraft propulsion systems than the commonly used ‘Thruster-specific Impulse’, Isp, which only includes the propellant mass. To achieve low system mass, high values for Issp are desired. The prevailing goal of advanced propulsion is to enable cost efficient space missions and extended exploration of the solar system up to interstellar missions.
Literature - 23 - Wiley J. Larsson and James R. Wertz (editors), 1995; ”Space Mission Analysis and Design”. Chapter 17: Spacecraft Propulsion Systems. Published jointly by Microcosm, Inc.; Torrance, California and Kluwer Academic Publishers Dodrecht/Boston/London. Philip G. Hill and Carl R. Peterson, 1992; ”Mechanics and Thermodynamics of Propulsion”. Chapters 10-12 and 14. Addison-Wesley Publishing Company, New York. George P. Sutton and A. Wiley, 1992; ”Rocket Propulsion Elements: An Introduction to the Engineering Rockets”. Sixth Edition, Interscience Publication, John Wiley & Sons, Singapore. Robert H. Frisbee; “Advanced Space Propulsion for the 21 st Century” Journal of Propulsion and Power, Vol.19, No. 6,November-December 2003 Peter Erichsen, 1997; ”Performance Evaluations of Spacecraft Propulsion Systems in Relation to Mission Impulse Requirements” Proceedings of the Second European Spacecraft Propulsion Conference, 27-29 May, 1997 (ESA SP-398, Aug. 1997) Peter Erichsen, 2003 “Directions of Potential Increase in Impulse Performance of Spacecraft Propulsion Systems”, Proceedings 10-IWCP, La Specia, Italy, Sept. 2003
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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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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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S.3 Basic Equation of Thrust - 3- B
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S.4 Basic Rocket Equation Total Vel
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Test - 9-
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Rocket propulsion device basic part
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Kinetic energy in the expelled mass
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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
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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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Diaphragm Tank - 27-
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Advantages Simplicity and reliabili
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Bipropellant Systems (Operate) - 31
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