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1. (WO2010113171) A MOBILE MISSILE LAUNCH SYSTEM AND METHOD THEREOF
Latest bibliographic data on file with the International Bureau   

Pub. No.: WO/2010/113171 International Application No.: PCT/IN2010/000018
Publication Date: 07.10.2010 International Filing Date: 11.01.2010
Chapter 2 Demand Filed: 02.12.2010
IPC:
F41A 23/34 (2006.01) ,F41A 23/36 (2006.01) ,F41A 23/42 (2006.01) ,F41F 3/04 (2006.01) ,F41F 3/052 (2006.01) ,F42B 39/22 (2006.01)
[IPC code unknown for ERROR IPC Code incorrect: invalid subclass (B=>S)!][IPC code unknown for ERROR IPC Code incorrect: invalid subclass (B=>S)!][IPC code unknown for ERROR IPC Code incorrect: invalid subclass (B=>S)!]
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
41
WEAPONS
F
APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
3
Rocket or torpedo launchers
04
for rockets
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
41
WEAPONS
F
APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
3
Rocket or torpedo launchers
04
for rockets
052
Means for securing the rocket in the launching apparatus
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
42
AMMUNITION; BLASTING
B
EXPLOSIVE CHARGES, e.g. FOR BLASTING; FIREWORKS; AMMUNITION
39
Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
22
Locking of ammunition in transport containers
Applicants:
GURUPRASAD, Siddalingappa [IN/IN]; IN (UsOnly)
KATTI, Shreedhar, Aravind [IN/IN]; IN (UsOnly)
GOUD, Alasani Prasad [IN/IN]; IN (UsOnly)
WAGHMARE, Vikas, Narayan [IN/IN]; IN (UsOnly)
KUMAR, Sanjay [IN/IN]; IN (UsOnly)
GUPTA, Atul [IN/IN]; IN (UsOnly)
KHIRE, Ravindra, Sudhakar [IN/IN]; IN (UsOnly)
SANTOSH, Tushar, Kant [IN/IN]; IN (UsOnly)
GAUTAM, Bimal [IN/IN]; IN (UsOnly)
RAM, Paras [IN/IN]; IN (UsOnly)
DIRECTOR GENERAL, DEFENCE RESEARCH & DEVELOPMENT ORGANISATION [IN/IN]; Ministry of Defence Govt. of India, Room No.348 B-Wing, DRDO Bhawan Rajaji Marg New Delhi 110 105, IN (AllExceptUS)
Inventors:
GURUPRASAD, Siddalingappa; IN
KATTI, Shreedhar, Aravind; IN
GOUD, Alasani Prasad; IN
WAGHMARE, Vikas, Narayan; IN
KUMAR, Sanjay; IN
GUPTA, Atul; IN
KHIRE, Ravindra, Sudhakar; IN
SANTOSH, Tushar, Kant; IN
GAUTAM, Bimal; IN
RAM, Paras; IN
Agent:
RANGAPPA, Paramenahalli, Himantharaju, Dodda; K&S Partners #4121/B, 6th Cross 19A Main, HAL II Stage [extension] Bangalore 560 038 Karnataka, IN
Priority Data:
00648/DEL/200930.03.2009IN
00684/DEL/200931.03.2009IN
00685/DEL/200931.03.2009IN
00703/DEL/200906.04.2009IN
Title (EN) A MOBILE MISSILE LAUNCH SYSTEM AND METHOD THEREOF
(FR) SYSTÈME DE LANCEMENT DE MISSILE MOBILE ET PROCÉDÉ ASSOCIÉ
Abstract:
(EN) 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.
(FR) L'invention concerne un système de lancement, et plus particulièrement un système de lancement mobile pour des missiles. Le système de lancement de missile mobile comprend un véhicule (14) comportant une structure de châssis conçue pour supporter le système de lancement ; un cadre de montage (16) comprenant une armature prédéfinie montée sur la structure de châssis ; une pluralité de mécanismes de coulissement montés à l'extrémité arrière du cadre de montage (16) ; une pluralité de lanceurs (43) montés sur ladite poutre (22) et une pluralité de missiles (11) renfermés dans les lanceurs (43) ; une pluralité de contenants (42) renfermant lesdits lanceurs (43) et reliés aux socles de pointage (32, 34) pour un déplacement linéaire ; et une pluralité d'unités d'appui (27) venant en butée contre l'extrémité arrière des lanceurs (43) et qui sont conçues pour se déplacer de manière linéaire afin de transférer des forces de réaction depuis lesdits missiles (11) vers le sol.
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Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IS, JP, KE, KG, KM, KN, KP, KR, KZ, LA, LC, LK, LR, LS, LT, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PE, PG, PH, PL, PT, RO, RS, RU, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW
African Regional Intellectual Property Organization (ARIPO) (BW, GH, GM, KE, LS, MW, MZ, NA, SD, SL, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Office (AM, AZ, BY, KG, KZ, MD, RU, TJ, TM)
European Patent Office (EPO) (AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, SE, SI, SK, SM, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, ML, MR, NE, SN, TD, TG)
Publication Language: English (EN)
Filing Language: English (EN)