A miniature solid-propellant rocket motor has been developed to impart a specific motion to an object deployed in space. This rocket motor effectively eliminated the need for a cold-gas thruster system or mechanical spin-up system. A low-energy igniter, an XMC4397, employing a semiconductor bridge was used to ignite the rocket motor. The rocket motor was ground-tested in a vacuum tank to verify predicted space performance and successfully flown in a Sandia National Laboratories flight vehicle program.
Miniature solid propellant rocket motor
1997
8 pages
Report
Keine Angabe
Englisch
A miniature solid propellant rocket motor
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British Library Conference Proceedings | 1997
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