Deployable heat shield and deceleration structure for...

Aeronautics and astronautics – Spacecraft – Reusable or returnable

Reexamination Certificate

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C244S171700, C244S172600

Reexamination Certificate

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07837154

ABSTRACT:
An apparatus for heat shielding and deceleration of a spacecraft comprises an unfoldable shield of individual panels made of a high temperature resistant fiber reinforced ceramic and pivotally mounted on the outer structure of the spacecraft. An unfolding ring slides axially along the body of the spacecraft. The panels are pivotally connected to the unfolding ring by compression struts acting as toggle levers. Tension springs pull the unfolding ring axially along the spacecraft body to toggle out the compression struts so as to outwardly pivotally deploy the panels. The unfoldable shield can be arranged on the forward end or the rear end of the spacecraft relative to its flight direction upon entry into the atmosphere.

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patent: 6735842 (2004-05-01), Wildenrotter et al.
patent: 7669802 (2010-03-01), Dorman
patent: 691 01 021 (1994-05-01), None

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