Unmanned aircraft
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Description
FIG. 1 is a perspective view of the aircraft;
FIG. 2 is a front view of the aircraft;
FIG. 3 is a rear view of the aircraft;
FIG. 4 is a top view of the aircraft;
FIG. 5 is a bottom view of the aircraft; and,
FIG. 6 is a side view of the aircraft.
Referenced Cited
U.S. Patent Documents
Other references
D314366 | February 5, 1991 | Waaland et al. |
3438597 | April 1969 | Kasper |
5082204 | January 21, 1992 | Croston |
5337975 | August 16, 1994 | Peinemann |
- Jane's all the World's Aircraft, 1995-1996, p. 616 Northrop Grumman B-2A. Jane's all the World's Aircraft, 1982-83, p. 808, IML-3 Addax-S, Supersonic Fighter.
Patent History
Patent number: D382851
Type: Grant
Filed: May 28, 1996
Date of Patent: Aug 26, 1997
Assignee: Lockheed Martin Corporation (Bethesda, MD)
Inventors: Eric D. Knutson (Lancaster, CA), Joseph M. Wurts (Valencia, CA), Michael H. Pohlig (Leona Valley, CA)
Primary Examiner: Kay H. Chin
Application Number: 0/55,000
Type: Grant
Filed: May 28, 1996
Date of Patent: Aug 26, 1997
Assignee: Lockheed Martin Corporation (Bethesda, MD)
Inventors: Eric D. Knutson (Lancaster, CA), Joseph M. Wurts (Valencia, CA), Michael H. Pohlig (Leona Valley, CA)
Primary Examiner: Kay H. Chin
Application Number: 0/55,000
Classifications
Current U.S. Class:
Horizontal Stabilizer Conforms To And Continues Wing Or Fuselage Configuration, E.g., Lifting Body Type (D12/333);
Aircraft, Spacecraft, Or Fuselage (D12/319)
International Classification: 1207;
International Classification: 1207;