Neospace, Inc.

États‑Unis d’Amérique

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Capsule spacecraft emergency landing system

      
Numéro d'application 13323699
Numéro de brevet 08690104
Statut Délivré - en vigueur
Date de dépôt 2011-12-12
Date de la première publication 2012-07-12
Date d'octroi 2014-04-08
Propriétaire NEOSPACE, INC. (USA)
Inventeur(s) Hudson, Gary C.

Abrégé

A method of landing a capsule-spacecraft having a crew compartment containing crew, light cargo, and whatever other elements are associated with crew safety and comfort during emergency recovery, such as survival equipment and a service component including any propulsion components, heat shield, heavier structure, or other equipment not directly connected with the crew component. In the event of a propulsion system failure, the crew compartment component is immediately separated from the service component, either by automatic or crew action. One or more parachutes are then deployed by rapid methods, such as rocket extraction, from the crew compartment. Because the space craft is separated into two parts the weight of the parachutes is reduced in proportion as the weight of the crew compartment is to the total capsule-spacecraft.

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