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

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<strong>S.1</strong>1 Electrical <strong>Propulsion</strong><br />

- 18-<br />

An Electric <strong>Propulsion</strong> system is a mass expulsion system in which electric energy is used <strong>to</strong><br />

create or augment the kinetic energy in the expelled mass. Consequently electric power will be<br />

of main interest in the performance evaluation of such systems.<br />

Kinetic Energy of Ejected Matter<br />

Power of the Jet<br />

Power Input<br />

1 2<br />

E jet = m pve<br />

[Ws]<br />

2<br />

dE 1 o<br />

jet 2 ve<br />

P jet = = mve<br />

= F<br />

dt 2 2<br />

2 P o<br />

jet ve<br />

ve<br />

P = = m = F<br />

η 2η<br />

2η<br />

where η is the power conversion efficiency.<br />

[W]<br />

[W]

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