1 / 22

SEMINAR ON “GUIDED MISSILES”

SEMINAR ON “GUIDED MISSILES”. SUBMITTED BY:-. NAME :- SHANKHADEEP BHATTACHARYA REGD. N O. :- 0901223305 ROLL NO. :- 09ME050. DEPART MENT OF MECHANICAL ENGINEERING KRUPAJAL ENGINEERING COLLEGE PUBASASAN KAUSALYAGANGA BHUBANESWAR. INTRODUCTION.

artan
Download Presentation

SEMINAR ON “GUIDED MISSILES”

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. SEMINAR ON “GUIDED MISSILES” SUBMITTED BY:- NAME:- SHANKHADEEP BHATTACHARYA REGD. NO.:- 0901223305 ROLL NO.:- 09ME050 DEPART MENT OF MECHANICAL ENGINEERING KRUPAJAL ENGINEERING COLLEGE PUBASASAN KAUSALYAGANGA BHUBANESWAR

  2. INTRODUCTION Guided Missiles, usually containing conventional or nuclear explosives, guiding flight towards a target either by remote control or by internal mechanisms. Guided missiles vary widely in size and type, ranging from large strategic ballistic missiles with nuclear warheads to small, portable rockets carried by foot soldiers. Principle of operation:- Tracking Guidance Flight

  3. TYPESOFMISSILES V1 & V2 A)SURFACE  TO SURFACE MISSILE 1. V-1 & V-2. 2. LAND BASED STRATEGIC MISSILE. 3.SEA BASED STRATEGICAL MISSILE. 4.CRUISE MISSILE. 5.TACTICAL MISSILE. B)AIR LAUNCHED MISSILE C)SURFACE TO AIR MISSILE Land Based Sea Based Cruise Tactical SAM ALM

  4. GUIDANCE SYSTEM TYPES OF GUIDANCE SYSTEMS MAJOR GUIDANCESYSTEMS REMOTE CONTROL BEAM RIDING LASER GUIDANCE ACTIVE RADAR HOMING WIRE GUIDED MISSILE INFRARED HOMING LONG RANGE NAVIGATION (LORAN) GLOBAL POSITIONING SYSTEM OPTICAL GUIDANCE

  5. TRACKING SYSTEM • TOW TRACKING SYSTEM • TVM TRACKING SYSTEM

  6. TOW TRACKING SYSTEM Tube-launched, Optically-tracked, Wire command-link Guided Missile System MISSILE WEIGHT:   TOW 2A: 47.1 lbs;   TOW 2B: 49.8lbs MISSILE LENGTH:   46.1 in MIN. RANGE:   TOW 2A: 65 m;   TOW 2B: 200 m MAX. RANGE:   3,750 m LAUNCHER WEIGHT :   204.6 lb CREW:   2

  7. TVM TRACKING SYSTEM Track-via-missile  System

  8. FLIGHT SYSTEMS • Vectored Thrust (For missiles that are powered throughout the guidance phase of their flight). • Aerodynamic Maneuvering (wings, fins, canards, etc.).

  9. Aerodynamic Maneuvering

  10. MISSILE COMPONENTS

  11. MOST COMMON TYPES OF WARHEAD MISSILES • Anti-Satellite Missile • Anti-Ship Missile • Anti-Tank Missile • Fire & Forget Missile • Ballistic Missile • Intercontinental Ballistic Missile

  12. ANTI-SATELLITE MISSILE Anti-satellite weapons (ASATs) are weapons designed to be used against artificial satellites. U.S. ASM-135 ASAT  missile

  13. ANTI-SHIP MISSILE An Anti-ship missile(AShM) is a militarymissile designed for use against navalsurface ships. RGM-84 Harpoon

  14. ANTI-TANK MISSILE An Anti-tank guided missile (ATGM) is a missile primarily designed to hit and destroy tanks. An alternative name is Anti-tank guided weapon (ATGW). FGM-148 Javelin

  15. FIRE & FORGET MISSILE Fire and forget is the military term for a type of missile which does not require further guidance after launch such as illumination of the target, and can hit its target without the launcher being in line of sight of the target. Nag missileof the Indian Armed Forces

  16. BALLISTIC MISSILE A ballistic missile is a missile, usually with no wings or fins, with a prescribed course that cannot be altered after the missile has burn edits fuel, whereafter its course is governed by the laws of ballistics. Trident II SLBM

  17. Intercontinental Ballistic Missile An intercontinental ballistic missile, or ICBM, is a long-range ballistic missile using a ballistic trajectory involving a significant ascent and descent, including sub-orbital flight. LGM- 25C Titan II

  18. ADVANTAGES OF GUIDED MISSILES • Missile combat employment is completely autonomous (“fire and forget”) • Missile flexible flight trajectories • High supersonic speed at a whole trajectory • High effectiveness in case of strong electronic and fire counter measures • High level of mobility • Minimal crew

  19. DISADVANTAGES OF GUIDED MISSILES • Missiles can be destroyed in flight (either with Defender missiles or with a well-timed smart bomb detonation) • Missiles have to rely on the ground-based radar for guidance • Nuclear missiles make plants, soil and rain radioactive

  20. CONCLUSION • The growth in the technological know-how of guided missiles has been spurred by an international race for strategic supremacy and commercial aspects. The decreasing gap between the launching of missiles and satellites, the military warfare has assumed a new dimension in the form of electronic and push-button warfare. With the present advancement of technology, the possibility of 'offsetting' the 'monopoly' of the Western countries in the arms trade appears not too distant when the poorer Third world nations would turn to countries like India in the weapons market which India can gladly afford at reduced prices.

  21. THANK YOU

More Related