Supersonic aircraft with in-flight refueling system

Description

FIG. 1 is a top, front and left side perspective view of supersonic aircraft with in-flight refueling system, embodying our new design;

FIG. 2 is a left side elevational view thereof;

FIG. 3 is a front elevational view thereof;

FIG. 4 is a rear elevational view thereof;

FIG. 5 is a top plan view thereof;

FIG. 6 is a bottom plan view thereof; and,

FIG. 7 is a top, front and left side perspective view thereof with the wings shown in a folded position.

Claims

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

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Inventors:	Simonov; Mikhail P. (Moscow, RU), Merkulov; Viktor I. (Khabarovsk Territory, RU), Ivanov; Yury L. (Moscow, RU), Marbashev; Konstantin K. (Moscow, RU), Maranov; Aleksandr Y. (Khabarovsk Territory, RU), Klyagin; Anatoly S. (Moscow, RU), Chernov; Leonid G. (Moscow, RU)
Assignee:	Zakrytoe Actsionernoe Obshchestvo "Otdelenie morskikh sistem OKB im. P.O. Sukhogo" (Moscow, RU)
Appl. No.:	D/103,739
Filed:	April 22, 1999

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Current U.S. Class:	D12/342; D12/319; D12/333
Current International Class:	1207
Field of Search:	;D12/319-345 ;244/15,45A,12,5,52

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References Cited [Referenced By]

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U.S. Patent Documents

D317897	July 1991	Antonov et al.
D319042	August 1991	Babak et al.
D332080	December 1992	Sandusky, Jr. et al.
4643374	February 1987	Friederich
4896846	January 1990	Strom
5526999	June 1996	Meston

Foreign Patent Documents

	44033		Jan 1998		RU

Primary Examiner: Chin; Kay H.
Attorney, Agent or Firm: Oblon, Spivak, McClelland, Maier & Neustadt, P.C.