Patent ID: 6398158
Filing Date: 2002-06-04
Classification: B60V,B64C

Abstract:
A high altitude low flying platform hull, comprising:(a) a laminar flow airfoil, the laminar flow airfoil having a nose, the nose having a nose leading edge; (b) a first slab side, the first slab side having a first slab side leading edge and a first slab side trailing edge, the first slab side leading edge being serpentine; (c) a second slab side, the second slab side having a second slab side leading edge and a second slab side trailing edge, the second slab side leading edge being serpentine, the first slab side and the second slab side mate to the laminar flow airfoil, the first slab side leading edge and the second slab side leading edge intersect the nose leading edge; (d) a first fin, the first slab side trailing edge extending upward to create the first fin; and (e) a second fin, the second slab side trailing edge extending upward to create the second fin.