Patent Document ID: 4374493
Application ID: 06278818
Patent Flag: 1

Claim One:
1. A model rocket assembly comprising: (a) a rocket body having an internal rigid tube containing a solid fuel rocket motor and extending substantially the entire length of the rocket and defining a frame; (b) substantially circular spacer disks concentric to said tube and spaced along the length of said tube; (c) a plurality of ribs joined to the outer circumferences of said disks substantially spanning the length of the body of the rocket and defining a frame; (d) skin formed around the frame of ribs in substantially cylindrical configuration spanning the length of the rocket and defining an enclosed void; (e) the top portion of said rocket body defining an aerodynamic nose assembly; (f) aerodynamic fins joined at the base of the rocket body; (g) said body being defined as a plurality of body sections, each constructed of an internal rigid tube, at least two circular spacer disks coaxial to said tube, a plurality of ribs joined to the outer circumferences of said disks and a skin formed around the frame of ribs in substantially cylindrical configuration such that the sections may be joined together by fastening the circular spacer disk of one section to a disk of next adjacent section forming a continuous cylindrical rocket body.