High altitude low flying platform hull

High altitude low flying platform hull

A high altitude low flying platform hull, including a laminar flow airfoil, a first slab side, a second slab side, a first fin and a second fin. The laminar flow airfoil has a nose, the nose has a nose leading edge. The first slab side has a first slab side leading edge and a first slab side trailin...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: REEVES JOHN M. L
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIR-CUSHION VEHICLES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:A high altitude low flying platform hull, including a laminar flow airfoil, a first slab side, a second slab side, a first fin and a second fin. The laminar flow airfoil has a nose, the nose has a nose leading edge. The first slab side has a first slab side leading edge and a first slab side trailing edge. The first slab side has a serpentine or s-shaped first slab side leading edge. The second slab side has a second slab side leading edge and a second slab side trailing edge. The second slab side has a serpentine or s-shaped second slab side leading edge. The first slab side and second slab side mate to the laminar flow airfoil. The first slab side leading edge and second slab side leading edge intersect the nose leading edge. The first slab side trailing edge extends upward to create the first fin, and the second slab side trailing edge extends upward to create the second fin.