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Priority to ES101125UpriorityCriticalpatent/ES101125Y/en
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Publication of ES101125YpublicationCriticalpatent/ES101125Y/en
Launching device-satellites, characterized by being constituted by a cylindrical tubular body in the form of a fuselage in one of whose open ends there is a sealing means or plug representing a spatial capsule shape, which is projected into space by virtue of the pressure that the interior of the tubular body exerts a bellows located at the other end of the fuselage and integral thereto, as a platform, by striking said bellows on a rigid surface. (Machine-translation by Google Translate, not legally binding)