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

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- 13-<br />

S.9 Type of <strong>Propulsion</strong> <strong>Systems</strong><br />

The basic propulsion mathematical formulas presented have <strong>to</strong> be further expanded for<br />

<strong>to</strong>day's commonly used on-board spacecraft propulsion system types:<br />

Chemical <strong>Propulsion</strong> <strong>Systems</strong><br />

The energy <strong>to</strong> produce thrust is s<strong>to</strong>red in the propellant, which is released by chemical<br />

reactions and the propellant is then accelerated <strong>to</strong> a high velocity by expanding it in form<br />

of gas through a nozzle.<br />

Electric <strong>Propulsion</strong> <strong>Systems</strong><br />

The energy <strong>to</strong> produce thrust is not s<strong>to</strong>red in the propellant but has <strong>to</strong> be supplied from<br />

outside by an extra power source, e.g. nuclear, solar radiation receivers or batteries.<br />

Thrust is produced by:<br />

- expansion of hot gas (which is heated by electric current)<br />

- accelerating of charged particles in electric or magnetic fields <strong>to</strong> high expulsion<br />

velocities.

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