A MOBILE MISSILE LAUNCH SYSTEM AND METHOD THEREOF

THE PRESENT INVENTION RELATES TO LAUNCHING SYSTEM, MORE PARTICULARLY RELATES TO MOBILE LAUNCHING SYSTEM FOR MISSILES. THE MOBILE MISSILE LAUNCH SYSTEM COMPRISING A VEHICLE (14) HAVING A CHASSIS STRUCTURE ADAPTED TO CARRY THE LAUNCH SYSTEM; A MOUNTING FRAME (16) COMPRISING PREDETERMINED TRUSS FRAMEWO...

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Hauptverfasser:	KATTI, SHREEDHAR, ARAVIND, WAGHMARE, VIKAS, NARAYAN, SANTOSH, TUSHAR, KANT, KUMAR, SANJAY, RAM, PARAS, GUPTA, ATUL, GAUTAM, BIMAL, GURUPRASAD, SIDDALINGAPPA, GOUD, ALASANI PRASAD, KHIRE, RAVINDRA, SUDHAKAR
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS HEATING LIGHTING MECHANICAL ENGINEERING MOUNTINGS FOR SMALLARMS OR ORDNANCE WEAPONS
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Zusammenfassung:	THE PRESENT INVENTION RELATES TO LAUNCHING SYSTEM, MORE PARTICULARLY RELATES TO MOBILE LAUNCHING SYSTEM FOR MISSILES. THE MOBILE MISSILE LAUNCH SYSTEM COMPRISING A VEHICLE (14) HAVING A CHASSIS STRUCTURE ADAPTED TO CARRY THE LAUNCH SYSTEM; A MOUNTING FRAME (16) COMPRISING PREDETERMINED TRUSS FRAMEWORK MOUNTED ONTO THE CHASSIS STRUCTURE; PLURALITY OF SLIDING MECHANISMS MOUNTED AT REAR END OF THE MOUNTING FRAME (16): PLURALITY OF CANISTERS (43) MOUNTED ONTO SAID BEAM (22) AND PLURALITY OF MISSILES (11) ENSCONCED WITHIN THE CANISTERS (43); PLURALITY OF CONTAINERS (42) ENCLOSING SAID CANISTERS (43) AND ARE CONNECTED TO THE SADDLES (32,34) FOR LINEAR MOVEMENT; PLURALITY OF RESTING UNITS (27) ABUTTING TO REAR END OF THE CANISTERS (43) AND ARE ADAPTED TO MOVE LINEARLY TO TRANSFER REACTION FORCES FROM SAID MISSILES (11) TO GROUND.