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COMENGES GARRIGA FRANCISCO
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COMENGES GARRIGA FRANCISCO
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Application filed by COMENGES GARRIGA FRANCISCOfiledCriticalCOMENGES GARRIGA FRANCISCO
Priority to ES221372ApriorityCriticalpatent/ES221372A1/en
Publication of ES221372A1publicationCriticalpatent/ES221372A1/en
Improvements in the descents of rocket aircraft, characterized in that in the cylindrical body of the same or fuselage and approximately at its center of gravity presents planiform projections destined for that the point of attachment or subjection for its propulsion, going said cylindrical body formed by two parts with turn in the "nose" or prow of the aircraft under a through axis in which an elastic device is conditioned to be able to launch with sufficient force, once the ascensional route is finished to an extensible surface by means of which, and its opening will get a perfect descent. (Machine-translation by Google Translate, not legally binding)
ES221372A1955-04-231955-04-23Improvements in the aircraft-rocket descenses (Machine-translation by Google Translate, not legally binding)
ExpiredES221372A1
(en)
Equations for the longitudinal control of an aircraft in which the elevator aerodynamic balance varies with the speed at which the aircraft is longitudinally balanced
Expression for the ideal weight of shell fuselages(Ideal weight of axisymmetric fuselage shells, taking into account load distribution and cabin pressurization)