Prefabricated space station

Aeronautics and astronautics – Spacecraft – Reusable or returnable

Patent

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Details

244158R, B64G 110

Patent

active

048801860

ABSTRACT:
The improvements of the organization and operation has to do with an adhesive that temporarily bonds the internal surfaces of two flexible envelopes equidistantly spaced from each other over the entire surfaces facing each other, the space between the walls bonded together separates upon pressurization of a foam between the walls dispersed by a hollow perforated hoop tube to disperse the foam under pressure evenly, while acting as an anchor of the flexible double wall to the deployment cylinder interior and gas and plastic catalysts reservoir within the container, on the end of the container are flanges as standards for interconnecting modules, hatches, and space craft; multiple function of deployment container offering perimeter as protective shield.

REFERENCES:
patent: 3144219 (1964-08-01), Schnitzer
patent: 3169379 (1965-02-01), Black
patent: 3282533 (1966-11-01), Spain
patent: 3357142 (1967-12-01), Furrer et al.
"Small Space Stations Built Around Last-Stage Tankage", Kurt R. Stehling, Space/Aeronautics, pp. 45-47, Sep. 1960.

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