Aerodynamic braking device

Aeronautics and astronautics – Retarding and restraining devices – Friction brakes

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Details

244160, 244138R, B64G 162

Patent

active

051080460

ABSTRACT:
Aerodynamic braking device, intended in particular for decelerating a space object penetrating an atmosphere at high speed, essentially constituted by a circular ring (2) made from canvas, of general shape close to that of a truncated cone but whose cross-section through an axial plane exhibits an outward concavity, and by a supporting structure (6, 7, 8) designed to apply a tangential tensile stress to the said ring in an axial plane, and preferably comprising at least two parallel rigid rings (6, 7), between which the canvas ring is stretched, and struts (8) arranged in order to retain the distance between the two rigid rings by resisting the loads resulting from the tension of the canvas.

REFERENCES:
patent: 3118636 (1964-01-01), Kantrowitz et al.
patent: 3405887 (1968-10-01), Mixson
patent: 3433435 (1969-03-01), Alai
patent: 3604667 (1971-09-01), Moraes
patent: 3888175 (1975-06-01), Dusoe et al.
patent: 4817895 (1989-04-01), Scott et al.
patent: 4832288 (1989-05-01), Kendall et al.
patent: 4856432 (1989-08-01), Synofzik
patent: 4860660 (1989-08-01), Synofzik et al.
patent: 4903918 (1990-02-01), Park et al.
Journal of Spacecraft and Rockets, vol. 4, No. 6, Jun. 1967, pp. 720-725, J. A. Alai, "Tension String Structure for Planetary Entry Vehicles".

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