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  Start of GV Modifications

October 29, 2003
Greenville, South Carolina

Click on the thumbnail images to see a larger version (larger image size in KB listed with each thumbnail).

File Type/Size   Description
Click to enlarge
JPG, 76KB
Lockheed Martin personnel installing support jigs and removing rivets from the forward section of the GV top fuselage in preparation for the installation of the forward upper crown section.
Click to enlarge
JPG, 69KB
View of the GV wing/body "joint" section with the wing-to-body fairing removed.
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JPG, 86KB
A view of the GV nose looking toward the back of the plane. The forward section jacking and shoring equipment is shown, along with a yellow securing strap. The aircraft radome is also up, showing the interior of the nose section.
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JPG, 54KB
The doubler to be installed along with the tripler fuselage as part of the forward upper crown section. Once the doubler and tripler have been installed, the upper optical view port and forward fuselage aperture plates and hard points will be cut into and installed within the coubler/tripler section. Jack Fox of NCAR/ATD/Design and Fabrication Services (DFS) is shown peeking above the middle section of the doubler, and Ken Hodge (Lockheed Martin HIAPER Project Engineer) is holding up the right side of the doubler.
Click to enlarge
JPG, 55KB
The tripler to be installed on the forward upper fuselage as part of the forward upper crown section. The tripler will be installed on top of the doubler. Jim Southwell of Lockheed Martin is shown in the left side of this picture.

 

 

 

 

 

 

 

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Support and operation of HIAPER is a partnership between the National Science Foundation and the National Center for Atmospheric Research PO Box 3000, Boulder CO 80307
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