Translation and locking mechanism in missile
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United States of America Patent
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-
Nov 4, 2003
Grant Date -
N/A
app pub date -
Apr 9, 2002
filing date -
Jun 4, 1999
priority date (Note) -
Expired
status (Latency Note)
Importance
Abstract
A translation and locking mechanism for a projectile that is lying in a standby position within a rocket motor in a missile, wherein the projectile is translated with respect to the rocket motor by means of a pyrotechnic charge before the rocket motor is ignited. The rear end of the projectile includes at least one radially spring biased lock and the front part of the rocket motor includes an internal circumferential groove that the at least one lock snaps into when the at least one lock is translated to the groove.
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