A rocket nozzle assembly is provided for operatively coupling to a rocket motor. The assembly includes a nozzle insert structure having a converging-diverging passageway with a throat region. First and second thrust control cylinders are parallel to each other and rotatable about respective axes transverse...http://www.google.es/patents/US20030046922?utm_source=gb-gplus-sharePatente US20030046922 - ROCKET NOZZLE ASSEMBLY HAVING ROTATABLE VARIABLE THRUST CONTROL CYLINDERS, AND ROCKET ASSEMBLY COMPRISING THE SAME
ROCKET NOZZLE ASSEMBLY HAVING ROTATABLE VARIABLE THRUST CONTROL CYLINDERS ...
Número de solicitud: 09/941,397 Número de publicación: US 2003/0046922 A1 Fecha de presentación: 29 Ago 2001 Patente emitida: US6651438 ( Fecha de emisión 25 Nov 2003)
