Title:
STRUCTURE OF EXTERNAL INSULATOR-TYPE SPACESHIP
Document Type and Number:
Japanese Patent JP2016118157
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide a space vehicle and a spaceship that enable low-cost locomotion to a space colony and that assure distinguished safety.SOLUTION: A takeoff is made using the rotation and revolution of the earth. Then, utilizing a body whose external part is composed of an insulator 1, the body is moved while the gravity and a magnetic force line are kept in a nonresistance state. An energy cost is maximally reduced, and use of electric power is limited for producing required compressed air. The compressed air is produced by a compressed air production device inside, stored in a compressed air tank, and discharged from an exhaust port. It is used only for a directional movement while keeping balance of a spaceship during takeoff and landing.SELECTED DRAWING: Figure 1
Inventors:
KOIZUMI HIROISA
Application Number:
JP2014258188A
Publication Date:
June 30, 2016
Filing Date:
December 22, 2014
Export Citation:
Assignee:
KOIZUMI HIROISA
International Classes:
F03H99/00; B64G1/26