Fundamentals Of Guided Missiles - DRDO
n, Head, Monographs division, who constantly interacted withme every step of the way and solved the many problems encountered, consideringthat this document covers science and technology in so many different areas ofspecialisation.SR Mohanxxii
List of AcronymsAAM or AAWACLOSAGCAMAMTIAPNASM or ASWATMAUM or ECDISMACEBWECMEDBAir-to-Air MissileAutomatic Command to Line-of-SightAutomatic Gain ControlAmplitude ModulationAirborne MTIAugmented Proportional NavigationAir-to-Surface MissileAnti-tank MissileAir-to-Underwater MissileCounter Clock WiseCast Double BaseCharacteristic EquationCircular Error ProbableCentre of GravityCumulative Kill ProbabilityCoherent OscillatorCommand to Line-of-Sight SystemCommand to Off the Line-of-SightConical Scan on Receive OnlyCentre of PressureCarboxyl Terminated Poly-ButadieneClock WiseContinuous WaveDirect ActionDynamic Error CompensationDigital Scene Area Matching and CorrelationExploding Bridge WireElectronic CountermeasuresExtruded Double Base
Fundamentals of Guided RFNAITUKELFLOSMAWElectro-Explosive DeviceExhaust Gas TemperatureExtremely High FrequencyElastomer Modified CDBExplosive Reaction ArmourElectrostatic GyroFuel-Air ExplosiveForward Looking InfraredFrequency ModulationFrequency Modulated Continuous WaveFibre Optic Laser GyroField-of-ViewFibre Re-inforced PlasticFrequency Shift KeyingGlobal Positioning SystemHigh ExplosiveHigh Explosive Squash HeadHigh FrequencyHydroxyl Terminated Poly-ButadieneInter Continental Ballistic MissilesInterrupted Continuous WaveIntermediate FrequencyInterrogation of Friend or FoeImaging Infrared SystemsInertial Navigation SystemIso Propyl NitrateInfra RedIntermediate Range Ballistic MissilesInfra Red Counter MeasureInhibited RFNAInternational Telecommunications UnionKinetic EnergyLow FrequencyLine-of-SightMisalignment Wavexxiv
List of AcronymsMCLOSMCTMEMSMFMGRMIRVMOPAMRBMMTIMTRNCNGNd RSWSACLOSSAMSAM or SAWSARSAUSAWManual Command to Line-of-SightMercury Cadmium TellurideMicro Electro Mechanical SystemMedium FrequencyMissile Guidance RadarMultiple Independently Targetable Re-entry VehicleMaster Oscillator Power AmplifierMedium Range Ballistic MissilesMoving Target IndicatorMissile Tracking RadarNitrocellulose and NitroglycerineNeodymium Yttrium Aluminium GarnetOnboard ComputerPotential EnergyPenta Erythritol TetranitrateProportional NavigationPlan Position IndicatorPure Proportional NavigationPulse Per SecondPulse Repitition FrequencyRadar Cross-SectionReference Cosine WaveRadio FrequencyRed Fuming Nitric AcidRate Integrating GyrosRing Laser GyroRotation of Sight LineRoot Sum of SquareReference Sine WaveSemi-Automatic Command to Line-of-SightSafety and Arming MechanismSurface-to-Air MissileSynthetic Aperture RadarSafety and Arming UnitSurface Acoustic Wavexxv
Fundamentals of Guided MissilesScramjetsSHFSHMS/N ratioSRBMSSKPSSMStaloSUM or SUWTBMTE CoolerTERCOMTFTIRTMTNTTPNTSFCTTRTVCTVMTWSUAM or UAWUDMHUHFUUM or UUWVCOVHFVLFVTSupersonic Combustion RamjetsSuper High FrequencySimple Harmonic MotionSignal-to-Noise RatioShort Range Ballistic MissilesSingle Shot Kill ProbabilitySurface-to-Surface MissileStable Local OscillatorSurface-to-Underwater MissileTheatre Ballistic MissilesThermo-Electric CoolerTerrain ComparisonTransfer FunctionTarget Illumination RadarTime MechanicalTriNitroTolueneTrue Proportional NavigationThurst Specific Fuel ConsumptionTarget Tracking RadarThrust Vector ControlTrack Via MissileTracle While ScanUnderwater-to-Air MissileUnsymmetrical Di-methyl HydrazineUltra High FrequencyUnderwater-to-Underwater MissileVoltage Controlled OscillatorVery High FrequencyVery Low Frequenc
ChAPTEr 4: PrOPULSION FUNDAMENTALS 57 4.1 Introduction57 4.2 Function 57 4.3 Velocity Profile of the Missile 58 4.4 Types of Engines 59 4.5 Igniters for Solid Rocket Motors 74 4.6 Jet Engines 77 4.7 Choice of Propulsion System 83 ChAPTEr 5: FUNDAMENT
Page 7 Follow us: Official Site, Telegram, Facebook, Instagram, Instamojo DRDO Successfully Test-Flights Surface-To-Air Missile Akash-NG’ DRDO Successfully Flight-Tests Indigenously Developed MPATGM DRDO Gives Licence To Laurus Labs To Make & Market 2-DG Army Inducts 10m Bridging System Developed By DRDO DRDO Successfully Flight-Tests ‘Agni P’ Ballistic Missile Off Odisha Coast
DRDO SUCCESSFULLY FLIGHT-TESTS INDIGENOUSLY DEVELOPED MPATGM FOR MINIMUM RANGE I n a major boost towards AatmaNirbhar Bharat and strengthening of the Indian Army, DRDO successfully flight-tested indigenously developed low weight, fire and forget Man-Portable Antitank Guided Missile (MPATGM) on 21 July 2021. The missile was launched from a man-
other DRDO laboratories. The launch was witnessed by the representatives of Indian Air Force (IAF). To capture flight data, ITR deployed a number of range stations like, electro-optical tracking system, radar and telemetry. The flawless performance of the entire weapon system has been confirmed by complete flight data captured by these systems .
instruments for doing some experiments, it is called a Sounding rocket. Rockets can also be used as missiles. Rockets are also used as launch vehicles. MISSILES Missiles are basically sub-orbital rockets. Some of the main types of missiles are as follows,
(NASA-CR- 120606) TEST REPORT SEPS SOLAR N75-1608' ARRAY ROOT SECTION HODEL (Lockheed Missiles and Space Co.) 50 p HC 3.75 CSCL 17A Unclas G3/44 09794 l'77 . manual assistance is required at both edges of the blanket to guide the panel fold line to the front of the containment box.-2-LOCKHEED MISSILES & SPACE COMPANY. INC.
Dayanand Saraswati University, Ajmer (Rajasthan). Undergone DRDO- orientation course of at Institute of Technology Management, Mussoorie (UK) during 02-20 Feb 2009. Attended a course on “Biostatistics for Life Sciences” under continuing Education Programme (CEP) of DRDO held at Defence Research Laboratory, Tezpur (Assam) during
We believe that the industries that figure in this compendium of "DRDO Industry Partnership - Synergy & Growth" has in fact enabled the establishment of a robust and competent defence industrial base in the country, who are better placed to undertake development related tasks in some of the cutting edge technology areas.
the welfarist objective assumed in modern Mirrleesian theory. In normative terms, the shift from the classical bene–t-based view to the dominant modern approach, which pursues so-called "endowment taxation," is quite substantial. Under the modern approach, an individual s income-earning ability is taken as a given, and as ability makes it .
