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.)
Brevets Aero Mecaniques SA
Original Assignee
Brevets Aero Mecaniques SA
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 Brevets Aero Mecaniques SAfiledCriticalBrevets Aero Mecaniques SA
Publication of ES247202A1publicationCriticalpatent/ES247202A1/es
Development of electrically initiated escape system components- ignition elements t 12 e 2, t 19 e 1, t 14 e 3, t 19 e 2, xm 21, xm 22, and xm 42- pulse generators xm 10, xm 11, and xm 15(Electric ignition element testing for use in propellant actuated escape systems)
Propulsion system diffusers for space flight simulation(Propulsion system diffuser criteria for testing rocket engines under simulated space flight conditions)