View
250
Download
4
Tags:
Embed Size (px)
Citation preview
Weapon Propulsion and Weapon Propulsion and ArchitectureArchitecture
Naval Weapons SystemsNaval Weapons Systems
Learning ObjectivesLearning Objectives
Comprehend gravity, impulse, and Comprehend gravity, impulse, and reaction propulsionreaction propulsionComprehend factors involved in impulse Comprehend factors involved in impulse propulsion (explosive propellant train, burn propulsion (explosive propellant train, burn rate, interior ballistics)rate, interior ballistics)Know the different types of reaction Know the different types of reaction propulsion systemspropulsion systemsComprehend basic principles of fluid Comprehend basic principles of fluid dynamicsdynamicsComprehend basic weapons architectureComprehend basic weapons architecture
Why is this important?Why is this important?
Evolution of WarfareEvolution of Warfare– Fists, sticks, and stonesFists, sticks, and stones– Spears and Bow/ArrowSpears and Bow/Arrow– 2020thth Century brought guns Century brought guns
Before fought in big formations (out mass enemy)Before fought in big formations (out mass enemy)
– Machine guns and cannonsMachine guns and cannonsIncreased need for dispersionIncreased need for dispersion
– Grenades and explosive shellsGrenades and explosive shells
In Desert Storm the allies decimated the Iraqi ranks and infrastructure from the air and sea before the troops ever entered the scene. When troops did move in, the Iraqi's were confused, hungry and demoralized. Many surrendered and those few that didn't were quickly killed.
IntroductionIntroduction
Every weapon requires some form of Every weapon requires some form of propulsion to deliver it to its intended propulsion to deliver it to its intended target.target.
Propulsion systems are based on Propulsion systems are based on Newton’s Third Law: Newton’s Third Law: For every action For every action there is an equal and opposite reaction.there is an equal and opposite reaction.
Types of PropulsionTypes of Propulsion
Propulsion Types can be divided into two Propulsion Types can be divided into two categories:categories:– 1) Energy Source1) Energy Source
Compression of Liquids/GassesCompression of Liquids/GassesChemical ReactionChemical ReactionEffect of GravityEffect of Gravity
– 2) Method of Launch2) Method of LaunchGravity - a bombGravity - a bombImpulse - a projectileImpulse - a projectileReaction - a missileReaction - a missile
Gravity PropulsionGravity Propulsion
Simple: Uses the force of gravity to get the weapon to the target.
Used in: - All free fall and glide bombs - Torpedoes launched from aircraft (until it submerges)
Gravity BombsGravity Bombs
MK-20 RockeyeMK-20 Rockeye– Free fall cluster bombFree fall cluster bomb– Over 27,000 dropped during Over 27,000 dropped during Desert stormTanks and Desert stormTanks and armored vehiclesarmored vehicles
AGM-62 WalleyeAGM-62 Walleye– Television guided glide bombTelevision guided glide bomb– 2000’ version “Fat Albert”2000’ version “Fat Albert”– Used during VietnamUsed during Vietnam
MK-46 TorpedoMK-46 Torpedo
Impulse LaunchingImpulse LaunchingChemical ReactionChemical Reaction
Impulse PropulsionImpulse Propulsion
Projectile is ejected from a container by Projectile is ejected from a container by means of an initial impulse.means of an initial impulse.
Explosive Propellant Train:Explosive Propellant Train:
PrimerPrimer
1
IgniterIgniter
2
Propellant PowderPropellant Powder
3
PropellantsPropellants
Smokeless Powders or Gunpowder's:Smokeless Powders or Gunpowder's:
– All are designed to produce large volumes All are designed to produce large volumes of gases at a controlled rate. of gases at a controlled rate.
– Rate is based on the maximum pressure Rate is based on the maximum pressure that can be withstood by the gun barrel, that can be withstood by the gun barrel, casing, etc.casing, etc.
Burn Rate Controlling FactorsBurn Rate Controlling Factors- - controls the pressure generated by controls the pressure generated by
the propellantthe propellant
Size and shape of the powder grainSize and shape of the powder grain
Web thickness; amount of propellant Web thickness; amount of propellant between burning surfaces of the grain.between burning surfaces of the grain.
Chemical burn rate constant of the Chemical burn rate constant of the propellant materialpropellant material
Percentage of volatile material present.Percentage of volatile material present.
Burning RatesBurning Rates
The Burn Rate increases as both the The Burn Rate increases as both the pressure and temperature rise.pressure and temperature rise.Classification by variation in burn rate:Classification by variation in burn rate:– DegressiveDegressive: As it burns, the burning surface area : As it burns, the burning surface area
decreasesdecreases– NeutralNeutral:: The burning surface area remains The burning surface area remains
constantconstant– ProgressiveProgressive: Burning surface area increases as : Burning surface area increases as
it burns.it burns.
Interior BallisticsInterior Ballistics
Action Inside a Gun.Action Inside a Gun.– Ignited propellant creates pressure within the Ignited propellant creates pressure within the
chamber that forces the projectile down the chamber that forces the projectile down the barrel.barrel.
Gun BarrelGun Barrel
ProgressiveProgressive
NeutralNeutralDegressiveDegressive
PressurePressure
Propulsion Propellent Burning GrainsPropulsion Propellent Burning Grains
Degressive burning Grains: Degressive burning Grains:
BallBall PelletPellet SheetSheet
– StripStrip CordCord
Propulsion Propellent Burning GrainsPropulsion Propellent Burning Grains
Neutral Burning Grains:Neutral Burning Grains:– Single PerforatedSingle Perforated
– Star PerforatedStar Perforated
**
Propulsion Propellant Burning GrainsPropulsion Propellant Burning Grains
Progressive Burning Grains:Progressive Burning Grains:– Multi-PerforatedMulti-Perforated
– RosetteRosette
Reaction LaunchReaction LaunchCompression of Compression of Liquids/GassesLiquids/Gasses
PropellantsPropellants
Compressed Air / Gas:Compressed Air / Gas:– Used to eject missiles or torpedoes from Used to eject missiles or torpedoes from
submarines.submarines.– Easily controllable; doesn't harm weaponsEasily controllable; doesn't harm weapons– Problem: Problem: Compressor machinery to maintain Compressor machinery to maintain
a supply of compressed gas.a supply of compressed gas.
Liquid FuelsLiquid Fuels
More powerful than solid fuelsMore powerful than solid fuels
High volatilityHigh volatility
Can’t be stored for long periodsCan’t be stored for long periods
Reaction PropulsionReaction Propulsion
Weapons employing reaction-type Weapons employing reaction-type propulsion obtain thrust by creating a propulsion obtain thrust by creating a pressure differential in the medium they pressure differential in the medium they operate in, i.e. air or water.operate in, i.e. air or water.
Examples include:Examples include:– Rockets, MissilesRockets, Missiles– Cruise MissilesCruise Missiles– Turbo-jet, and Ram Jet enginesTurbo-jet, and Ram Jet engines
Reaction PropulsionReaction Propulsion
Development of Thrust in a Rocket Development of Thrust in a Rocket Motor:Motor:
Pressure is BalancedPressure is Balanced Burning Propellant along the insideBurning Propellant along the insideof the casing exerts pressure in allof the casing exerts pressure in alldirections at once, until a nozzle isdirections at once, until a nozzle isfitted a one end.fitted a one end.
Pressure is Un-BalancedPressure is Un-BalancedForward VelocityForward Velocity
ThrustThrust
Bernoulli’s TheoryBernoulli’s Theory
ConvergentConvergent DivergentDivergent
Pressure IncreasesPressure IncreasesVelocity DecreasesVelocity Decreases
Pressure DecreasesPressure DecreasesVelocity IncreasesVelocity Increases
Gas Turbine EngineGas Turbine Engine
TurbojetTurbojet
LM2500LM2500
DC 10DC 10
TurbopropTurboprop
RamjetRamjet
Low-Supersonic Mach 3 to Mach 5Low-Supersonic Mach 3 to Mach 5
JP-4JP-4
ScramjetScramjet
Hypersonic Mach 5 to Mach 20Hypersonic Mach 5 to Mach 20
HydrogenHydrogen
SOLID FUELSOLID FUEL
AdvantagesAdvantages– SimpleSimple– ReliableReliable– Unlimited SpeedUnlimited Speed– Any medium/vacuumAny medium/vacuum– Few moving partsFew moving parts– Full thrust at takeoffFull thrust at takeoff– Store fully fueledStore fully fueled– Ready to fire!Ready to fire!
DisadvantagesDisadvantages– No boosterNo booster– Not restartableNot restartable
LIQUID FUELLIQUID FUEL
AdvantagesAdvantages– RestartableRestartable– Practically unlimited Practically unlimited
speedspeed– Any medium/vacuumAny medium/vacuum– Full thrust on take-offFull thrust on take-off– Less need for booster Less need for booster
than air breatherthan air breather– Staged with liquid/solid Staged with liquid/solid
rocketsrockets
DisadvantagesDisadvantages– Many moving partsMany moving parts– ComplexComplex– Cost and Safety Cost and Safety
issuesissues– More VolatileMore Volatile
TURBOJETTURBOJET
AdvantagesAdvantages– Large static thrustLarge static thrust– Oxygen from airOxygen from air– Common fuels (JP-Common fuels (JP-
4,5,&8)4,5,&8)– Thrust independent of Thrust independent of
speedspeed
DisadvantagesDisadvantages– Basic design lacks Basic design lacks
improvements in improvements in efficiency and powerefficiency and power
TURBOFANTURBOFAN
AdvantagesAdvantages– Quieter than turbojetQuieter than turbojet– More efficient at More efficient at
subsonic airspeeds subsonic airspeeds than turbojet (typically than turbojet (typically at higher altitudes)at higher altitudes)
DisadvantagesDisadvantages– More complexMore complex– Large diameter engineLarge diameter engine– More blades=more More blades=more
susceptible to FODsusceptible to FOD
TURBOPROPTURBOPROP
AdvantagesAdvantages– Very high fuel Very high fuel
efficiency at slow efficiency at slow speedsspeeds
– High shaft power to High shaft power to weight ratioweight ratio
DisadvantagesDisadvantages– Limited top speedsLimited top speeds– NoisyNoisy– Complex prop Complex prop
driveshaftdriveshaft
RAMJET/SCRAMJETRAMJET/SCRAMJET
AdvantagesAdvantages– SimpleSimple– No wearing partsNo wearing parts– Oxygen from airOxygen from air– LightweightLightweight– Inexpensive to build and Inexpensive to build and
operateoperate– Common fuelsCommon fuels– Efficient at high Efficient at high
speeds/altitudesspeeds/altitudes– SupersonicSupersonic– Hydrogen fuel (for Hydrogen fuel (for
SCRAMJET)SCRAMJET)
DisadvantagesDisadvantages– In Developmental stagesIn Developmental stages– Cooling/Intake difficultiesCooling/Intake difficulties– No thrust at restNo thrust at rest– Must be combined with Must be combined with
another type of engine to another type of engine to get up to speed.get up to speed.
– Minimum Mach NumberMinimum Mach Number– Hydrogen fuel (for Hydrogen fuel (for
SCRAMJET)SCRAMJET)– EXPENSIVE fuel sourceEXPENSIVE fuel source
Questions?Questions?