Device for absorbing the lateral forces of the jet flow separation acting on the nozzle of a rocket engine

The device has a control actuator (106) e.g. electrical type actuator, with ends (106a, 106b) hinged to a rocket and an anchor structure (104). A rigid connecting rod secured to ends (102a, 102b) of a strut (102) includes a tube presenting circumferential slots. A separating unit separates the rod f...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BRANCHET, CHRISTELLE, EVEN, PHILIPPE, BEAUVERGER, PHILIPPE, MILLON, FREDERICK
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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