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A model space vehicle having a fixed circular wing, streamlined fuselage, fins with booms attached thereto all efficiently configured to result in an article possessing suitable aerodynamic properties to enable it to glide smoothly through the air for a substantial period of time and substantial dis

A model space vehicle having a fixed circular wing, streamlined fuselage, fins with booms attached thereto all efficiently configured to result in an article possessing suitable aerodynamic properties to enable it to glide smoothly through the air for a substantial period of time and substantial distance relative to its size and weight.

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1. A model space craft suitable for gliding comprising:a fixed circular wing means for providing lift, having a topside and an underside and a thickness, said underside of said fixed circular wing being more convex than said topside of said circular wing; said fixed circular wing having an approxima

1. A model space craft suitable for gliding comprising:a fixed circular wing means for providing lift, having a topside and an underside and a thickness, said underside of said fixed circular wing being more convex than said topside of said circular wing; said fixed circular wing having an approximate diameter 8 times that of its thickness; a streamlined fuselage which extends fore and aft along a longitudinal axis about which said model space craft can assume a roll attitude; connecting means extending from said underside of said circular wing, protruding downward and rearward and attached to a fore section location on said streamlined fuselage; said streamlined fuselage having a tapered profile toward the aft section thereof; said streamlined fuselage being reinforced using a lightweight stress bearing strut extending the length of said fuselage as measured from a point of said fuselage where said fuselage meets said circular wing, to a rear of said fuselage; a pair of fins protruding from opposite sides of said streamlined fuselage and positioned and fixed at a first end to said aft of said streamlined fuselage, and extending outward radially at an angle of approximately 40 degrees from the vertical axis and rearward at an angle of approximately 30 degrees to the vertical; each said fin being approximately 4 times wider than their thickness and having a streamlined profile to promote effective stability to said model space craft; each said fin at its upper end supports a boom at a height above the horizontal plane of said circular wing so as to avoid said booms being subjected to the turbulence which is produced by airflow over said circular wing; the relative dimensions of the length, width and thickness of each said boom is approximately 5 times as long as it is wide and approximately 4 times wider than it is thick; each said boom comprises a flat underside and a domed topside with a rearward taper; each said boom lies on a horizontal plane parallel to the horizontal plane of said fixed circular wing with a slight tilt of between about 1.0 degrees and 1.5 degrees clockwise viewed from a left side of said model space ship; a ballast is positioned in the foresection of the circular wing so as to achieve a center of gravity point which is approximately two thirds the diameter of said circular wing, measured from the leading edge of said circular wing.