Tactical aircraft decoy, conjugal tandem design
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Description
FIG. 1 is a front perspective view of the invention;
FIG. 2 is a side view of the invention;
FIG. 3 is a top view of the invention;
FIG. 4 is a bottom view of the invention;
FIG. 5 is a front end view of the invention; and,
FIG. 6 is a rear end view of the invention.
Referenced Cited
U.S. Patent Documents
Other references
D198881 | August 1964 | King et al. |
D203902 | February 1966 | Raymes |
D220983 | June 1971 | Webb et al. |
D220985 | June 1971 | Webb et al. |
5494239 | February 27, 1996 | Giacomel |
- Popular Science, Jul. 1986, p. 37, Aerospace plane.
Patent History
Patent number: D381938
Type: Grant
Filed: Aug 31, 1995
Date of Patent: Aug 5, 1997
Assignee: Northrup Grumman Corporation (Los Angeles, CA)
Inventors: Stephen P. Grossman (El Segundo, CA), Barnaby S. Wainfan (Long Beach, CA)
Primary Examiner: Kay H. Chin
Attorneys: Terry J. Anderson, Karl J. Hoch, Jr.
Application Number: 0/43,312
Type: Grant
Filed: Aug 31, 1995
Date of Patent: Aug 5, 1997
Assignee: Northrup Grumman Corporation (Los Angeles, CA)
Inventors: Stephen P. Grossman (El Segundo, CA), Barnaby S. Wainfan (Long Beach, CA)
Primary Examiner: Kay H. Chin
Attorneys: Terry J. Anderson, Karl J. Hoch, Jr.
Application Number: 0/43,312
Classifications
Current U.S. Class:
Bearing Or Fifth Wheel (D12/161);
Aircraft, Spacecraft, Or Fuselage (D12/319)
International Classification: 1207;
International Classification: 1207;