Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rheinmetall Air Defence AG
Original Assignee
Werkzeugmaschinenfabrik Oerlikon Buhrle AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Werkzeugmaschinenfabrik Oerlikon Buhrle AGfiledCriticalWerkzeugmaschinenfabrik Oerlikon Buhrle AG
Publication of ES202836A1publicationCriticalpatent/ES202836A1/en
A rocket projectile with solid propulsion load of a piece characterized in that in the hollow space of the propellant charge is arranged concentrically a straight body that extends over the entire length thereof and that only partially fills the hollow space. (Machine-translation by Google Translate, not legally binding)
ES0202836A1951-10-251952-04-04A rocket proyectile (Machine-translation by Google Translate, not legally binding)
ExpiredES202836A1
(en)
A proyectil-cohete with propulsion load in head, applicable to parts striped artilleras or not (Machine-translation by Google Translate, not legally binding)
A projectile with gradual and prolonged transmission of explosive effect to incendiary effect (Machine-translation by Google Translate, not legally binding)