S.1 Spacecraft Propulsion Systems Chapter 1: Introduction to ...
S.1 Spacecraft Propulsion Systems Chapter 1: Introduction to ...
S.1 Spacecraft Propulsion Systems Chapter 1: Introduction to ...
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S.7 Solid Propellant Mo<strong>to</strong>r<br />
- 48-<br />
The solid propellant mo<strong>to</strong>r consists of a mo<strong>to</strong>r case, containing a propellant grain, a nozzle<br />
and an igniter. The main characteristics and performance are as follows:<br />
- Main performance<br />
- Advantages<br />
- Disadvantages<br />
In general, solid propulsion mo<strong>to</strong>rs can only deliver their <strong>to</strong>tal impulse potential in one<br />
firing, because off-modulation is not possible. Therefore the usage of solid propulsion is<br />
restricted <strong>to</strong>:<br />
- Orbit change (e.g. apogee or perigee maneuver)<br />
- Impart acceleration (e.g. liquid reorientation maneuvers, separation maneuvers)