Supersonic aircraft with in-flight refueling system

Transportation – Aircraft – spacecraft – or fuselage – Plural distinct engine air intakes on fuselage flanks or...

Design Patent

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Details

CD12S319000, CD12S333000

Design Patent

active

D0439876

CLAIM:
The ornamental design for supersonic aircraft with in-flight refueling system, as shown and described.

REFERENCES:
patent: D. 317897 (1991-07-01), Antonov et al.
patent: D. 319042 (1991-08-01), Babak et al.
patent: D. 332080 (1992-12-01), Sandusky, Jr. et al.
patent: 4643374 (1987-02-01), Friederich
patent: 4896846 (1990-01-01), Strom
patent: 5526999 (1996-06-01), Meston
patent: 44033 (1998-01-01), None

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