ES221372A1 - Improvements in the aircraft-rocket descenses (Machine-translation by Google Translate, not legally binding) - Google Patents

Improvements in the aircraft-rocket descenses (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES221372A1
ES221372A1 ES221372A ES221372A ES221372A1 ES 221372 A1 ES221372 A1 ES 221372A1 ES 221372 A ES221372 A ES 221372A ES 221372 A ES221372 A ES 221372A ES 221372 A1 ES221372 A1 ES 221372A1
Authority
ES
Spain
Prior art keywords
aircraft
translation
machine
rocket
legally binding
Prior art date
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.)
Expired
Application number
ES221372A
Other languages
Spanish (es)
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.)
COMENGES GARRIGA FRANCISCO
Original Assignee
COMENGES GARRIGA FRANCISCO
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 COMENGES GARRIGA FRANCISCO filed Critical COMENGES GARRIGA FRANCISCO
Priority to ES221372A priority Critical patent/ES221372A1/en
Publication of ES221372A1 publication Critical patent/ES221372A1/en
Expired legal-status Critical Current

Links

Abstract

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)
ES221372A 1955-04-23 1955-04-23 Improvements in the aircraft-rocket descenses (Machine-translation by Google Translate, not legally binding) Expired ES221372A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES221372A ES221372A1 (en) 1955-04-23 1955-04-23 Improvements in the aircraft-rocket descenses (Machine-translation by Google Translate, not legally binding)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES221372A ES221372A1 (en) 1955-04-23 1955-04-23 Improvements in the aircraft-rocket descenses (Machine-translation by Google Translate, not legally binding)

Publications (1)

Publication Number Publication Date
ES221372A1 true ES221372A1 (en) 1955-06-16

Family

ID=65627849

Family Applications (1)

Application Number Title Priority Date Filing Date
ES221372A Expired ES221372A1 (en) 1955-04-23 1955-04-23 Improvements in the aircraft-rocket descenses (Machine-translation by Google Translate, not legally binding)

Country Status (1)

Country Link
ES (1) ES221372A1 (en)

Similar Documents

Publication Publication Date Title
GB884128A (en) Improvements in or relating to flying bodies for supersonic speeds
ES221372A1 (en) Improvements in the aircraft-rocket descenses (Machine-translation by Google Translate, not legally binding)
FR1154259A (en) Rudder for vehicles, especially boats and airplanes
BULYGINA et al. Lower surface geometry determination for balancing supersonic aircraft
SCHAFFER The load stresses on aircraft at the speed of sound and supersonic speeds investigated by flight simulation
MALICKY 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
CH369925A (en) Aircraft actual flight speed calculator
KUKLEV Calculation of the momentum coefficients of both natural damping and effectiveness of air rudders in flying platforms during hovering flight
KUCHERMANN Characteristic configurations for supersonic aircraft with specific flight requirements
ES67724U (en) Improved glider airplane toy (Machine-translation by Google Translate, not legally binding)
QUARANTA Review of the development of aircraft toward supersonic speeds, discussing design, costs and airports
CA636063A (en) Probes for use in refuelling aircraft in flight
FR1254696A (en) Airplane, especially for supersonic flight speeds
ES260949A1 (en) Improvements in aeroplanes
ES234709A1 (en) Disposition of the elements of propulsion to jet in flying bodies (Machine-translation by Google Translate, not legally binding)
AU121107B2 (en) Improvements ina cargo carrying body foran airplane
AU204172B2 (en) Improvements in or relating to aircraft flight controls
RAJPERT Problems of airfield construction with respect to the accommodation of modern airplanes and helicopters
KERSLAKE Requirements for cabin environments in civil and military supersonic aircraft
AU203090B2 (en) Improvements in jet propulsion for aircraft and control means therefor
GABRIELLI Expression for the ideal weight of shell fuselages(Ideal weight of axisymmetric fuselage shells, taking into account load distribution and cabin pressurization)
FR1227746A (en) Improvements to the sensors used to refuel an aircraft in flight
AU1453955A (en) Improvements in or relating to aircraft flight controls
ES62172U (en) Toy jet airplane (Machine-translation by Google Translate, not legally binding)
FR1113078A (en) Device for controlling the forces exerted in flight on the airfoil of an airplane and other flying machines