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:
Aug. 12, 2014
Filed:
Jan. 11, 2010
Siddalingappa Guruprasad, Maharashtra, IN;
Shreedhar Aravind Katti, Maharashtra, IN;
Alasani Prasad Goud, Maharashtra, IN;
Vikas Narayan Waghmare, Maharashtra, IN;
Sanjay Kumar, Maharashtra, IN;
Atul Gupta, Maharashtra, IN;
Ravindra Sudhakar Khire, Maharashtra, IN;
Tushar Kant Santosh, Maharashtra, IN;
Bimal Gautam, Maharashtra, IN;
Paras Ram, Maharashtra, IN;
Siddalingappa Guruprasad, Maharashtra, IN;
Shreedhar Aravind Katti, Maharashtra, IN;
Alasani Prasad Goud, Maharashtra, IN;
Vikas Narayan Waghmare, Maharashtra, IN;
Sanjay Kumar, Maharashtra, IN;
Atul Gupta, Maharashtra, IN;
Ravindra Sudhakar Khire, Maharashtra, IN;
Tushar Kant Santosh, Maharashtra, IN;
Bimal Gautam, Maharashtra, IN;
Paras Ram, Maharashtra, IN;
Director General, Defence Research & Development Organisation, Rajaji Marg, IN;
Abstract
The present invention relates to launching system, more particularly relates to mobile launching system for missiles. The mobile missile launch system comprising a vehicle () having a chassis structure adapted to carry the launch system; a mounting frame () comprising predetermined truss framework mounted onto the chassis structure; plurality of sliding mechanisms mounted at rear end of the mounting frame (); plurality of canisters () mounted onto said beam () and plurality of missiles () ensconced within the canisters (); plurality of containers () enclosing said canisters () and are connected to the saddles () for linear movement; plurality of resting units () abutting to rear end of the canisters () and are adapted to move linearly to transfer reaction forces from said missiles () to ground.