The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Jun. 16, 1987
Filed:
Jul. 28, 1986
Robert E Betts, Huntsville, AL (US);
Jerrold H Arszman, Huntsville, AL (US);
The United States of America as represented by the Secretary of the Army, Washington, DC (US);
Abstract
A recoilless rocket launcher including a rocket launch tube which is resintly coupled to a support member. Points of contact to the gunner who fires the rocket from a rocket launch tube are to the shoulder and the hand which grips a hand grip which is part of the firing mechanism integrally attached to the support member. The resilient coupling for support member is comprised of a resilient material selected from the group consisting of a butene-diolefin copolymer, rubber, plastic, leather, or fiberous paper. The resilient material disposed in spaced relation adjacent opposite ends of the support member resiliently couples the support member to the launch tube. The nonrigid coupling effects the transfer mechanisms to result in a time offset, extended reaction time, and a reduced total impressed impulse transferable to the gunner prior to rocket exiting the rocket launch tube. This described action is accomplished by the resilient coupling, and in an advanced embodiment, sliding means to allow the rocket launch tube to freely slide in the support member also permits a significant delay and a reduction in the forces that can be transferred directly to the gunner to thereby derive benefits including improved personal comfort to the gunner, enhancement of confidence level in system, and a significant improvement in the expected accuracy of the rocket launched to a target from a shoulder fired rocket launcher.