|
The ornamental design for radar cross section measurement pylon terminating device, as shown and described. |
FIG. 1 is a perspective view of the radar cross section measurement pylon terminating device;
FIG. 2 is a side view of the radar cross section measurement pylon terminating device;
FIG. 3 is a top view of the radar cross section measurement pylon terminating device;
FIG. 4 is a bottom view of the radar cross section measurement pylon terminating device;
FIG. 5 is a front view of the radar cross section measurement pylon terminating device;
FIG. 6 is a rear view of the radar cross section measurement pylon terminating device; and,
FIG. 7 is a partial cross-sectional view taken along line 7--7 of FIG. 4.
Patent | Priority | Assignee | Title |
Patent | Priority | Assignee | Title |
4990923, | Jun 29 1989 | The Boeing Company | Test pylon having low radar cross section |
5075681, | Jan 28 1991 | Lockheed Martin Corporation | Radar cross-section model support and positioning apparatus |
5311191, | Nov 02 1992 | Grumman Aerospace Corporation | Automatic anechoic chamber calibrator |
5337016, | Jul 09 1993 | Boeing Company, the | Method and apparatus for traveling wave attenuation measurement |
Executed on | Assignor | Assignee | Conveyance | Frame | Reel | Doc |
Mar 31 1995 | DRINHAUS, MARK T | Lockheed Corporation | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 007425 | /0120 | |
Apr 06 1995 | Lockheed Corporation | (assignment on the face of the patent) | / | |||
Jan 28 1996 | Lockheed Corporation | Lockheed Martin Corporation | MERGER SEE DOCUMENT FOR DETAILS | 015386 | /0365 |
Date | Maintenance Fee Events |
Date | Maintenance Schedule |