Aircraft system for reduced observer visibility
An aircraft apparatus is disclosed that has a fuselage boom (102) having proximal (110) and distal (103) ends, a wing (108) coupled to a proximal end (110) of the fuselage boom (102) and at least one transparent stabilizer (104, 106) coupled to a distal end (103) of the fuselage boom (102).
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | An aircraft apparatus is disclosed that has a fuselage boom (102) having proximal (110) and distal (103) ends, a wing (108) coupled to a proximal end (110) of the fuselage boom (102) and at least one transparent stabilizer (104, 106) coupled to a distal end (103) of the fuselage boom (102). |
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