USD180890S - Guided missile - Google Patents

Description

United States Patent Ofifice" Des. 180,890 Patented Sept. 3, 1957 GUIDED MISSILE nter A. B

William Hu oyd, Kensington, Md., assignor to the United Sta es of America as represented by the Secretary of the Navy Application May 6, 1949, Serial No. 2,502

Term of patent 14 years (Cl. D7 1-1) Des. 180,890

PAGE 2 Fig. l is a perspective view of a guided missile as it appears when seen obliquely from above and at the front;

Fig. 2 is an inverted perspective view of the guided missile when seen from a position below and at the front;

Fig. 3 is a perspective view of the guided missile as it appears when seen obliquely from above and at the rear, and

Fig. 4 is a side elevation of the guided missile.

The design for a guided missile is characterized by the superstructure on the payload, and the tapered, sweptback wings that project from its sides virtually fiush with the top surface thereof and, further, by the empennage under the aft end of the payload component and the shroud ring.

What is claimed is: The ornamental design for a guided missile, substantially as shown and described.

References Cited in the file of this patent Popular Mechanics, December 1947, page 129, figure in lower right hand corner of page.

Flight, October 5, 1944, pages 364 and 365, figure illustrated under Wasted Talent.

Air News, April 1942, page 6, Fig.: Avro-Manchester in center right of page (see empennage).

Images