Transport safety device in rocket launcher - involves locking bolt engaging in start tube recess

The rocket fits into a start tube (1) for launching, and in an area surrounded by the start tube is at least one radially movable locking component (11). In the start tube is at least one recess (12) in which the locking component can engage. The locking arrangement (14) works with a spring (18) so...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: RUEDIGER, MANFRED., 5210 TROISDORF, DE, GOERICKE, DETLEF., 5000 KOELN, DE
Format: Patent
Sprache:eng ; ger
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:The rocket fits into a start tube (1) for launching, and in an area surrounded by the start tube is at least one radially movable locking component (11). In the start tube is at least one recess (12) in which the locking component can engage. The locking arrangement (14) works with a spring (18) so that the point (13) of the locking component (11) stands outwards over the periphery of the rocket. When the rocket is introduced into the start tube, the locking component together with its point is pushed backwards. The locking arrangement (14) has a pyrotechnical power component (19) which, when initiated, causes the point of the locking component to be drawn in so far that the engagement of the locking component in the recess of the start tube is nullified. The locking component (11) is a bolt, and the recess (12) in which it engages is a radial hole. USE/ADVANTAGE - To improve the fixture of a military rocket in its launching or start tube.