초록 ▼

An anti tip-off device for rocket rockets adapted for collapsible tube-inbe launchers is provided. The dual-diameter launch tube requires stabilization of the rocket within the larger diameter tube. The anti tip-off device has two segments which together form a hollow cylinder which fits over the no

An anti tip-off device for rocket rockets adapted for collapsible tube-inbe launchers is provided. The dual-diameter launch tube requires stabilization of the rocket within the larger diameter tube. The anti tip-off device has two segments which together form a hollow cylinder which fits over the nose section of a standard high explosive anti-armor rocket. A sliding surface is located around the circumference of the cylinder to provide support for the rocket during transit of the larger launch tube. The surface contact prevents the rocket from wobbling or tipping during the rocket's transit of the launch tube. Alternately, permanently-bonded stabilizer legs or a bonded ring may be attached to the rocket to match the diameter of the larger launch tube. The anti tip-off device may be fabricated using any material suited to the launcher and rocket combination, including lexan, teflon, nylon, wood, or aluminum.

대표청구항 ▼

[ What is claimed as new and desired to be secured by Letters Patent of the United States is:] [1.] An anti tip-off device for a rocket launched from a collapsible tube-in-tube, dual diameter launcher having larger and smaller diameter tubes comprising:segment shells forming a cylindrical shape havi

[ What is claimed as new and desired to be secured by Letters Patent of the United States is:] [1.] An anti tip-off device for a rocket launched from a collapsible tube-in-tube, dual diameter launcher having larger and smaller diameter tubes comprising:segment shells forming a cylindrical shape having a hollow interior adapted to fit over a nose section of standard high explosive anti-armor rockets; anda sliding bearing surface attached to said segment shells and located around the circumference to provide a bearing surface during rocket transit of a larger diameter tube, said sliding bearing surface located longitudinally so that the distance from the bearing surface to the aft end of the rocket is the same distance as the internal length of the larger diameter launch tube.