Spin-stabilized lander

B - Operations – Transporting – 64 – G

Patent

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Details

B64G 1/24 (2006.01) B64C 25/00 (2006.01) B64G 1/00 (2006.01) B64G 1/22 (2006.01)

Patent

CA 2706719

The invention provides a novel, low-cost, spin-stabilized lander architecture capable (with appropriate system scaling tailored to the attributes of the target) of performing a soft- landing on a solar-system body such as Earth's Moon, Mars, Venus, the moons of Mars, Jupiter, Saturn, Uranus and Neptune, selected near-Earth and main-belt asteroids, comets and Kuiper belt objects and even large human-made objects, and also moving about on the surface of the target solar-system body after the initial landing in movement akin to hopping.

L'invention concerne une nouvelle architecture de module attérisseur gyro-stabilisé bon marché, capable (avec une mise à l'échelle du système adéquate personnalisée pour répondre aux attributs de la cible) d'exécuter un attérissage en douceur sur un corps du système solaire, tel que la lune, Mars, Vénus, les lunes de Mars, Jupiter, Saturne, Uranus et Nepture, certains astéroïdes proches de la Terre et certains astéroïdes de la ceinture principale, les comètes, et les objets se trouvant dans la ceinture de Kuiper, y compris des objets de grande taille fabriqués par l'homme, et de se déplacer autour de la surface du corps du système solaire ciblé après l'attérissage initial en un mouvement proche du saut.

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