SlideShare a Scribd company logo
CHINA RUSIA US
PL-21
 Mass : 270 kilogram (600 lb)
 Length : 5,5 meter (18 kaki)
 Diameter : 250–300 mm (9,8–11,8 in)
 Warhead : 6kg blast-frag, or expanding rod
(RF-fuse)
 Detonation mechanism : Active infrared,
laser proximity fuse(PL-5EII)
 Engine : Ramjet
 Wingspan 0.657m (PL-5B, PL-5C), 0.617m
(PL-5E)
 Operational range : 150 – 200 km
 Speed Mach 2.5
 Guidance Sistem : Actif radar with AESA
 Launch platform : Aircraft,
 Medium Range
R-77
 Mass : 175 kg (R-77), 190 kg (R-77-1)
 Length : 3.6 m (R-77), 3.71 m (R-77-1)
 Diameter : 200 mm
 Warhead : 22.5 kg HE fragmenting (R-77)
 Detonation mechanism Laser proximity fuse
 Engine Solid fuel rocket motor (R-77), air-
breathing ramjet (R-77-PD)
 Wingspan700 mm
 Operational range 80–100 km (R-77), 110 km
(R-77-1), 193 km (R-77M)
 Flight altitude : 5–25 km (16,000–82,000 ft)
 Speed Mach 4, Mach 5 for K-77PD (RVV-AE-
PD)
 Guidance system : Inertial with mid-course
update and terminal active radar
homing/infrared homing (R-77T)
 Launch platform : Aircraft:
 Medium Range
AIM 120-AMRAM
 Mass : 335 lb (152 kg)
 Length : 12 ft (3.7 m)
 Diameter : 7 in (180 mm)
 Warhead : High explosive blast-fragmentation
 Detonation mechanism : Active RADAR
Target Detection Device (TDD), Quadrant
Target Detection Device (QTDD) in AIM-120C-
6 – lots 13+
 Engine Solid-fuel rocket motor
 Wingspan20.7 in (530 mm) AIM-120A/B
 Operational range : AIM-120A/B: 55–75 km
(30–40 nmi), AIM-120C-5: >105 km (>57
nmi), AIM-120D (C-8): >160 km (>86 nmi)[6]
 Speed Mach : 4 (4,900 km/h; 3,045
mph)[citation needed
 Guidance system : inertial guidance, terminal
active radar homing
 Launch platform : Aircraft:
 Medium Range.
AIR TO AIR MISSILE (MEDIUM RANGE)
CHINA RUSIA US
DF-12 M20
 Type Short-range surface-to-air missile
System
 Country users : China
 Warhead : 480 kg
 System reaction time :10 sec.
 Armament : Two missiles in individual
container ready to fire
 Range missile : Minimum 100 km;
Maximum 280 km
 Guidance system : Inertial guidance and
INS with satellite guidance
 Radar and command station : Command
and control vehicle
9K720 ISKANDER-M/SS-26 STONE
 Missile Variants : Iskander-M; Iskander-E
(export)
 Mobility and Role : Road-mobile; surface-to-
surface short-range ballistic missile
 Designer/Producer : Machine-Building Design
Bureau
 Range : 400-500 km (Iskander-M); 280 km
(Iskander-E)
 Warhead Type and Weight : Nuclear and
conventional – 700 kg
 Guidance System/Accuracy : Inertial and
optical/10-30 m CEP (Iskander-M);
Inertial/30-70 CEP (Iskander-E)
 Stages/Propellant : One/Solid
 IOC/Retirement : 2006 (Iskander-M)/Not
Available Need updating by 2020
MGM-140 ATACMS
 Mass : 3,690 pounds (1,670 kg)
 Length : 13 feet (4.0 m)
 Diameter : 24 inches (610 mm)
 Maximum firing range: 190 mi (300 km)
 Wingspan55 inches (1.4 m)
 Flight ceiling : 160,000 ft (50 km)
 Speed : In excess of Mach 3 (0.6 mi/s; 1.0
km/s)
 Guidance System : GPS-aided inertial
navigation guidance
 Launch platform : M270, HIMARS.
BALISTIC MISSILE (TACTICAL MISSILE)
CHINA RUSIA US
DF-11
 Type : SRBM (Short Range Balistic Missile)
 Used by PRC
 Production history
 Manufacturer :Academy of Rocket Motors
Technology
 Specifications
 Mass 3,800 kg[1]
 Length 7.5-8.5 m[2]
 Diameter 0.86 m
 Warhead 500 kg: 2/10/20 kiloton nuclear
warhead, fuel-air explosive (FAE), chemical,
or submunition
 Engine single-stage solid-propellant rocket
 Operational range : DF-11:300+ km
 DF-11A:700+ km, DF-11AZT:600 km
 Guidance System :Astro-inertial guidance
(including ring-laser gyroscope) + Beidou
 Launch Platform : Road-mobile TEL
P-800 ONIKS (SS-N-26)
 Russian/NATO Designation P-800 Oniks (Land-
based Yakhont)/SS-N-26 Strobile Variants
BrahMos
 Mobility and Role :
 Surface-to-Surface Anti-Ship Cruise Missile
 Max Speed 3000 km/h
 Designer/Producer NPO Mashinostroyeniya
 Range 300km
 Warhead Type and Weight
 3000kg launch weight
 HE warhead; Armor-Piercing Warhead Yield
 200kg HE warhead;
 250 kg Armor-piercing warhead
 Guidance System/Accuracy
 1.5m CEP
 Satellite Guidance; Active Radar Seeker
 Cruise Altitude Max 14,000 m
 Propellant Solid-fuel Booster;
Liquid-Fuel Ramjet Sustainer
 IOC/Retirement :2002/Operational
 Status/Number of Units Operational/Unknown
 Launch Vehicles
 Nakat class missile ship; Yasen class
submarine;
 Bastion-P/Bastion-S ground-launch system
PGM-11 REDSTONE
BALISTIC MISSILE (SHORT RANGE)
 Mass : 61,207 pounds (27,763 kg) at ignition
 Length : 69.3 feet (21.1 m)
 Diameter : 5.83 feet (1.8 m)
 Blast yield :3.5 megatons of TNT (15 PJ) or 500
kilotonnes of TNT (2.1 PJ)
 thermonuclear warhead
 Engine : Rocketdyne North American Aviation
75–110 A-7
 78,000 pounds-force (350 kN) thrust at sea level
for 121 seconds
 Payload capacity : 6,305 pounds (2,860 kg)
 Propellant ethyl alcohol, liquid oxygen, hydrogen
peroxide
 Fuel capacity : alcohol: 11,135 pounds (5,051 kg),
liquid oxygen: 25,280 pounds (11,470 kg),
hydrogen peroxide: 790 pounds (360 kg)
 Operational range : 57.5 miles (92.5 km) to 201
miles (323 km)
 Flight altitude : 28.4 miles (45.7 km) peak
minimum to 58.7 miles (94.5 km) peak maximum
 Boost time: 97 seconds to 117 seconds
 Speed Mach : 5.5 maximum at re-entry interface
 Guidance System : Ford Instrument Company
ST-80 inertial guidance
 Steering System : Carbon jet vanes, air rudders,
spatial air jet nozzles, air vanes
 Accuracy : 300 metres (980 ft) CEP
 Launch platform :Guided missile platform
launcher M74
CHINA RUSIA US
DF-21
- Mass 14,700 kilograms (32,400 lb)
- Length 10.7 metres (35 ft)
- Diameter 1.4 metres (4.6 ft)
- Warhead 600kg: 1, or 5-6 (improved variant)[1]
200-300-500 kt nuclear[2]
- Engine Solid fueled
- Operational range :1,770 km (1,100 mi) (DF-
21/DF-21A), 1,700 km (1,100 mi) (DF-21C)
- 1,500 km (930 mi; 810 nmi) (DF-21D ASBM)[4]
- Speed Mach : 10
- Guidance System:Inertial + terminal active radar
guidance
- Accuracy :DF-21 700m, DF-21A 50m, DF-21B
10m CEP (with BeiDou Navigation Satellite
System and active radar)
- Launch Platform : Mobile launcher
SSC - 8
 Country of origin : Russia
 Entered service : 2018
 Crew : 3 men
 Number of missiles : 4
 Weight : ~ 40 t
 Length : 13.25 m
 Width : 3.51 m
 Height : 3.94 m
 Missile length (including booster) : ~ 8 m
 Missile diameter : 0.53 m
 Wing span : ~ 3 m
 Missile weight : ~ 2 300 kg
 Warhead weight : 400 ~ 500 kg
 Warhead type : Nuclear
 Range : 2 000 ~ 2 500 (?)
 CEP : ~ 5 m
Mobility :
 Engine : YaMZ-846 diesel
 Engine power : 500 hp
 Maximum road speed :70 km/h
 Range : 1 000 km – 5000 Km
 Maneuverability
 Gradient :45%
 Side slope : 30%
 Vertical step : ~ 0.6 m
 Trench : 2 m
 Fording : 1.4 m
AGM-86
 Overall length: 19.82 m (65.0 ft)
 Span: 2.74 m (9.0 ft)
 Weight: 49,800 kg (109,800 lb)
 Empty weight: 3,125 kg (6,889 lb)
 Core Diameter: 2.44 m
 Maximum range: 2,400 km (1,500 mi)
 Ceiling: 480 km (300 mi)
 Guidance: Inertial
 Maximum speed: 17,740 km/h (11,020 mph)
 Engines: Vernier: 2x Rocketdyne LR101-NA; 4.5 kN
(1000 lbf)
 Warhead : One W49 warhead on Mk. 2 reentry
vehicleMass 3,150 pounds (1,430 kg)
 Length 20 ft. 9 in. (6.3 m)
 Diameter 24.5 inches (620 mm)[
 Warhead W80 thermonuclear weapon (AGM-86B)
 conventional warhead (AGM-86C)
 AUP warhead (AGM-86D)
 Warhead weight : 908kg (AGM-86C Block 0)
 1362kg (AGM-86C Block 1)
 1,200 lb class advanced unitary penetrating
warhead (AGM-86D)
 Engine : Williams International
 F107-WR-101 turbofan engine
 600 lbf (2.7 kN) thrust
 Wingspan 12 feet (3.7 m)
 Guidance system : AGM-86B: Litton inertial nav
system element with TERCOM, AGM 86C: Litton
INS element integrated with GPS
 Launch platform : Boeing B-52H Stratofortress
BALISTIC MISSILE (MEDIUM RANGE)
CHINA RUSIA US
JL-2
 Type : SLBM (Submarine Launched Balistic
Missile)
 Place of origin :People's Republic of China
 Service history
 In service Active as of 2015
 Used by People's Liberation Army Navy
 Specifications
 Mass : 42,000 kilograms (93,000 lb)[2]
 Length : 13 metres (43 ft)[2]
 Warhead : 1 nuclear warhead[3]
 Blast yield : 1 megaton of TNT (4.2 PJ)[4]
 Propellant : Solid-fuel rocket
 Operational Range : 7,200 km (4,500 mi)[5]
 Guidance System : Astro-inertial[4] with
Beidou
 Launch Platform : Type 094 submarine
SS-19 STILLETO
 Length (m) : 17.2
 Body diameter (m) : 2.5
 Fueled weight (t) : 86.3
 Engine Designation : RD-0233 / RD-0234,
 RD-0235 (14/15D113)
 Vernier Engine Designation RD-0236 (15D114)
 Bus Engine Designation Third Stage RD-0237
 Fuel : UDMH
 Oxidizer : Nitrogen Tetroxide
 Payload (t) : 4.350
 Total length (m) : 24.3
 Warhead (m) : 21.1
 Missile Diameter (m) : 2.50
 Launch Weight (t) : 103.4 - 105.6
 Fuel Weight (t) : 93.1
 Range (km) : 10,000
MINUTEMAN III
 Berat : 78,000 lb (35,300 kg)
 Panjang : 59 ft 9.5 in (18.2 m)
 Diameter : 5 ft 6 in (1.7 m) (1st stage)
 Hulu ledak : Nuclear W62, W78, or (2006-) W87
 Jenis Mesin : Three solid-propellant rocket
motors; first stage - Thiokol TU-122 (M-55);
second stage - Aerojet-General SR-19-AJ-1;
third stage - Aerojet/Thiokol SR73-AJ/TC-1
 Daya jelajah : 8,100 miles (13,000 km)
 Ketinggian terbang : 700 miles (1,120
kilometers)
 Kecepatan Approximately : 15,000 mph (Mach
23, or 24,100 km/h, or 7 km/s) (terminal phase)
 Sistem penuntun : Inertial
 Alat Peluncur : Silo
BALISTIC MISSILE (LONG RANGE)
CHINA RUSIA US
QW-2 VANGUARD 2
 Type MANPAD
 Service history 1990’s to present
 Used by China and Bangladesh
 Production history
 Produced : Since Mid 1990’s
Specifications
 Weight : 11.32 kg, 18 kg with launcher
 Length : 1.59 meter
 Detonation
 mechanism : Impact & Proximity
 Engine rocket
 Propellant : solid rocket
 Operational Range : 6 km maximum
 Flight ceiling : 3 km
 Flight altitude : 10 meter minimum
 Speed > 600 m/s
 Guidance System : Infrared homing
 Launch Platform : MANPADS, Type 95
SPAAA
PANTSIR (S1, S2 & S3)
 Armament : Twelve ground-to-air missile
launcher 57E6 / 57E6-E, two dual 2A38M 30
mm autocannon guns
 Country users : Iran, Iraq, Serbia, United Arab
Emirates, Jordan, Russia, Syria, Vietnam
 Designer Company : KBP Instrument Design
Bureau
 Accessories : Radio commands with IR or radio
direction finding, autonomous acquisition radar
and tracking radar
 Crew : 3 soldiers
 Radar System : Autonomous acquisition and
tracking radar 1RS2-1
 Range missile : 1 – 30 km
 Weight missile : 90 kg with container
MIM-104 PATRIOT (PAC3)
 Specifications (PAC-1)
 Mass : 700 kg (1,500 lb)
 Length : 5,800 mm (19 ft 0 in)
 Diameter : 410 mm (16 in)
 Warhead : M248 Composition B HE blast/
fragmentation with two layers of pre-formed
fragments and Octol 75/25 HE blast/
fragmentation
 Warhead weight : 200 lb (90 kg)
 Detonation mechanism : Proximity fuze
 Wingspan : 920 mm (3 ft 0 in)
 Propellant : Solid-fuel rocket
 Operational Range : PAC-3: 20 km against
ballistic missile, PAC-3 MSE: 35 km against
ballistic missile
 Flight altitude : 79,500 feet (24,200 m)
 Speed : PAC-1: Mach 2.8, PAC-2/PAC-3: Mach
4.1
 Guidance System : PAC-1: Radio command with
Track Via Missile semi-active homing, PAC-3: Ka
Band AESA seeker
 Launch Platform : Mobile trainable four-round
semi-trailer
SURFACE TO AIR MISSILE (SHORT RANGE)
CHINA RUSIA US
KS-1
 Weight: 900 kg
 Warhead: > 100 kg
 Length: 5.6 m
 Diameter: 0.4 m
 Speed: 1,200 m/s
 Maneuverability: > 20 g
 Maximum target speed: 750 m/s
 Maximum target maneuverability: > 5 g
 Maximum range: > 50 km
 Minimum range: 100 m
 Maximum altitude: > 25 km
 Minimum altitude: < 500 m
S-300 VM
 Operational Range : 200 (250) km against
MRBMs
 9M82M missile
 Type : Surface-to-air missile
 Place of origin : Russia
 Production history
 Designer : Almaz-Antey
 Designed 2000s
 Manufacturer : Almaz-Antey
 Produced : 2013-present
 Variants 9M82M, 9M83M
 Specifications (9M82M
 Operational Range :
200 kilometres (120 mi)
 Flight altitude :
30,000 metres (98,000 ft)
MIM-104 PATRIOT (PAC1 & PAC2)
 Specifications (PAC-1)
 Mass : 700 kg (1,500 lb)
 Length : 5,800 mm (19 ft 0 in)
 Diameter : 410 mm (16 in)
 Warhead : M248 Composition B HE blast/
fragmentation with two layers of pre-formed
fragments and Octol 75/25 HE blast/
fragmentation
 Warhead weight : 200 lb (90 kg)
 Detonation mechanism : Proximity fuze
 Wingspan : 920 mm (3 ft 0 in)
 Propellant : Solid-fuel rocket
 Operational Range : PAC-1: 70 km
 PAC-2: 96 km-160 km
 Flight altitude : 79,500 feet (24,200 m)
 Speed : PAC-1: Mach 2.8, PAC-2/PAC-3: Mach
4.1
 Guidance System : PAC-1: Radio command with
Track Via Missile semi-active homing, PAC-3: Ka
Band AESA seeker
 Launch Platform : Mobile trainable four-round
semi-trailer
SURFACE TO AIR MISSILE (MEDIUM RANGE)
CHINA RUSIA US
HG-9
 Mass :1300 kg
 Length : 6.8 m
 Warhead weight :180 kg
 Engine Two-stage solid propellant rocket
 Operational Range : 200 km (FD-2000
version) 250 km (HQ-9A version) 300+ km for
HQ-9B version
 Flight ceiling : 27 km, 41 km for HQ-9B
 Speed Mach : 4.2
 Guidance System Inertial guidance with mid-
course update and terminal active radar
homing
 Launch Platform : Taian TA580/TAS5380 8×8
transporter erector launcher (TEL)
 Type 052C destroyer
 Type 052D destroyer
 Type 055 destroy
S-500 PROMETHEUS
 S-500 launcher based on the BAZ-69069
chassis
 Country of origin : Russia
 Entered service : Expected in 2025
 Crew 3 men
 Weight 54 t
 Length ~ 14.5 m
 Width ~ 3 m
 Range of fire : 500 ~ 600 km
 Altitude of fire : ~ 40 km
 Mobility :
 Engine : diesel
 Engine power : 550 hp
 Maximum road speed ~ 70 km/h
 Range ~ 1 000 km
 Maneuverability
 Gradient 60%
 Side slope 30%
 Vertical step ~ 0.6 m
 Trench ~ 2 m
 Fording 1.7 m;
AN/TWQ-1 AVENGER
 Country of origin : United States
 Entered service : 1990
 Crew : 2 men
 Weight 4.3 t
 Length 4.95 m
 Width 2.49 m
 Height 2.64 m
 Missile length 1.52 m
 Missile diameter 0.07 m
 Missile weight 10.1 kg
 Warhead weight 3 kg
 Warhead type HE-FRAG
 Range of fire 4 - 8 km
 Altitude 3.5 - 3.8 km
 Guidance : Infrared homing
 Engine Detroit Diesel diesel
 Engine power 135 hp
 Maximum road speed 100 km/h
 Range 480 km
 Maneuverability
 Gradient 60%
 Side slope : 30%
 Vertical step : 0.5 m
 Trench : 0.5 m
 Fording : 0.75 - 1.5 m
SURFACE TO AIR MISSILE (LONG RANGE)
CHINA RUSIA US
YJ-12B
 Country of origin China
 Crew ~ 5
 Weight ~ 40 t
 Length ~ 16 m
 Width ~ 3 m
 Height ~ 3.5 m
 Warhead weight 200 kg
 Warhead type HE-FRAG
 Range of fire 400 ~ 500 km
 Guidance : Inertial with active radar homing
 Mobility
 Engine Deutz diesel
 Engine power : 544 hp
 Maximum road speed :70 km/h
 Range 650 km
 Maneuverability
 Gradient 40%
 Side slope : 20%
 Vertical step : 0.4 m
 Trench 2.5 m
 Fording 1.2 m
BAL
 Country of origin Russia
 Entered service 2004
 Crew 3 men
 Weight ~ 40 t
 Length ~ 12.8 m
 Width ~ 3 m
 Height ~ 3.6 m
 Missile length 4.4 m
 Missile diameter 0.42 m
 Wing span 1.33 m
 Missile weight 620 - 670 kg
 Warhead weight 145 kg
 Warhead type HE-FRAG
 Range of fire 130 / 260 km
 Engine YaMZ-846
 Engine power 500 hp
 Maximum road speed 70 km/h
 Range 1 000 km
 Maneuverability Gradient 45%
 Side slope 30%
 Vertical step ~ 0.6 m
 Trench 2 m
 Fording 1.4 m
BGM-109G GRYPHON
 Country of origin United States
 Entered service 1983
 Crew 3 men
 Number of missiles 4
 Weight 36 t
 Length 19.8 m
 Width 2.44 m
 Height ~ 3 m
 Missile length (without booster) 5.56 m
 Missile diameter 0.52 m
 Missile launch weight 1 200 kg
 Warhead weight 176 kg
 Warhead type Nuclear, 150 kT yield
 Range of fire 2 500 km
 CEP ~ 30 m
 Engine MAN D2866 KFG diesel
 Engine power 360 hp
 Maximum road speed 80 - 90 km/h
 Range ~ 800 km
 Maneuverability
 Gradient (with trailer) ~ 20%
 Fording ~ 1.2 m
COASTAL DEFENSE SYSTEM (ANTI SHIP MISSILE)

More Related Content

Similar to RUDAL.pptx

Design of fighter aircraft presentation
Design of fighter aircraft presentationDesign of fighter aircraft presentation
Design of fighter aircraft presentation
Dudekula Jamal
 
AAV or EFV iteration 2nd Infantry Antiaircraft Amphibious Modular Vehicle 35-...
AAV or EFV iteration 2nd Infantry Antiaircraft Amphibious Modular Vehicle 35-...AAV or EFV iteration 2nd Infantry Antiaircraft Amphibious Modular Vehicle 35-...
AAV or EFV iteration 2nd Infantry Antiaircraft Amphibious Modular Vehicle 35-...
Andrey F Engineer
 
AAV or EFV iteration 2nd Infantry FirePower Amphibious Modular Vehicle 1 36- ...
AAV or EFV iteration 2nd Infantry FirePower Amphibious Modular Vehicle 1 36- ...AAV or EFV iteration 2nd Infantry FirePower Amphibious Modular Vehicle 1 36- ...
AAV or EFV iteration 2nd Infantry FirePower Amphibious Modular Vehicle 1 36- ...
Andrey F Engineer
 
Anti ballistic missiles i
Anti ballistic missiles iAnti ballistic missiles i
Anti ballistic missiles i
Solo Hermelin
 
indian Airforce
indian Airforceindian Airforce
indian Airforce
kamal Mehta
 
Exclusive aircrafts.
Exclusive aircrafts.Exclusive aircrafts.
Exclusive aircrafts.
Trilochan K.
 
Fugro-Synergy_(2010)_Drillship-Brochure_FWS
Fugro-Synergy_(2010)_Drillship-Brochure_FWSFugro-Synergy_(2010)_Drillship-Brochure_FWS
Fugro-Synergy_(2010)_Drillship-Brochure_FWSErik-André Albrecht
 
Gaganyaan Test Vehicle TV-D1 Brochure.pdf
Gaganyaan Test Vehicle TV-D1 Brochure.pdfGaganyaan Test Vehicle TV-D1 Brochure.pdf
Gaganyaan Test Vehicle TV-D1 Brochure.pdf
Champs Elysee Roldan
 
Rockets and Missile Technology AEROSPACE.pptx
Rockets and Missile Technology AEROSPACE.pptxRockets and Missile Technology AEROSPACE.pptx
Rockets and Missile Technology AEROSPACE.pptx
PIYUSHNIGAM15
 
AAV or EFV iteration 2nd Infantry Fighting Amphibious Modular Vehicle 1 31- 3...
AAV or EFV iteration 2nd Infantry Fighting Amphibious Modular Vehicle 1 31- 3...AAV or EFV iteration 2nd Infantry Fighting Amphibious Modular Vehicle 1 31- 3...
AAV or EFV iteration 2nd Infantry Fighting Amphibious Modular Vehicle 1 31- 3...
Andrey F Engineer
 
Altus exertus-specification
Altus exertus-specificationAltus exertus-specification
Altus exertus-specification
patel170591
 
Ching kuo (idf) multirole fighter jet, taiwan
Ching kuo (idf) multirole fighter jet, taiwanChing kuo (idf) multirole fighter jet, taiwan
Ching kuo (idf) multirole fighter jet, taiwanhindujudaic
 
AAV or EFV iteration 2nd Infantry Amphibious Modular Tank 33 - 38 t with 17 -...
AAV or EFV iteration 2nd Infantry Amphibious Modular Tank 33 - 38 t with 17 -...AAV or EFV iteration 2nd Infantry Amphibious Modular Tank 33 - 38 t with 17 -...
AAV or EFV iteration 2nd Infantry Amphibious Modular Tank 33 - 38 t with 17 -...
Andrey F Engineer
 
Aircraft
AircraftAircraft
Aircraft
hanif miyanoor
 
Cn 235 persuader maritime patrol aircraft, spain
Cn 235 persuader maritime patrol aircraft, spainCn 235 persuader maritime patrol aircraft, spain
Cn 235 persuader maritime patrol aircraft, spainhindujudaic
 
Cutters And Aircraft
Cutters And AircraftCutters And Aircraft
Cutters And AircraftUSCGA
 
T129
T129T129
T129
Leonardo
 
DESIGN AND FABRICATION OF QUADCOPTER
DESIGN AND FABRICATION OF QUADCOPTERDESIGN AND FABRICATION OF QUADCOPTER
DESIGN AND FABRICATION OF QUADCOPTERPrasanna Achanti
 
Helicopter Kamov-32
Helicopter Kamov-32 Helicopter Kamov-32
Helicopter Kamov-32
Martin Gòmez-Palacio Duarte
 

Similar to RUDAL.pptx (20)

Design of fighter aircraft presentation
Design of fighter aircraft presentationDesign of fighter aircraft presentation
Design of fighter aircraft presentation
 
AAV or EFV iteration 2nd Infantry Antiaircraft Amphibious Modular Vehicle 35-...
AAV or EFV iteration 2nd Infantry Antiaircraft Amphibious Modular Vehicle 35-...AAV or EFV iteration 2nd Infantry Antiaircraft Amphibious Modular Vehicle 35-...
AAV or EFV iteration 2nd Infantry Antiaircraft Amphibious Modular Vehicle 35-...
 
AAV or EFV iteration 2nd Infantry FirePower Amphibious Modular Vehicle 1 36- ...
AAV or EFV iteration 2nd Infantry FirePower Amphibious Modular Vehicle 1 36- ...AAV or EFV iteration 2nd Infantry FirePower Amphibious Modular Vehicle 1 36- ...
AAV or EFV iteration 2nd Infantry FirePower Amphibious Modular Vehicle 1 36- ...
 
Anti ballistic missiles i
Anti ballistic missiles iAnti ballistic missiles i
Anti ballistic missiles i
 
indian Airforce
indian Airforceindian Airforce
indian Airforce
 
Exclusive aircrafts.
Exclusive aircrafts.Exclusive aircrafts.
Exclusive aircrafts.
 
Fugro-Synergy_(2010)_Drillship-Brochure_FWS
Fugro-Synergy_(2010)_Drillship-Brochure_FWSFugro-Synergy_(2010)_Drillship-Brochure_FWS
Fugro-Synergy_(2010)_Drillship-Brochure_FWS
 
Gaganyaan Test Vehicle TV-D1 Brochure.pdf
Gaganyaan Test Vehicle TV-D1 Brochure.pdfGaganyaan Test Vehicle TV-D1 Brochure.pdf
Gaganyaan Test Vehicle TV-D1 Brochure.pdf
 
tomohawk missile
tomohawk missiletomohawk missile
tomohawk missile
 
Rockets and Missile Technology AEROSPACE.pptx
Rockets and Missile Technology AEROSPACE.pptxRockets and Missile Technology AEROSPACE.pptx
Rockets and Missile Technology AEROSPACE.pptx
 
AAV or EFV iteration 2nd Infantry Fighting Amphibious Modular Vehicle 1 31- 3...
AAV or EFV iteration 2nd Infantry Fighting Amphibious Modular Vehicle 1 31- 3...AAV or EFV iteration 2nd Infantry Fighting Amphibious Modular Vehicle 1 31- 3...
AAV or EFV iteration 2nd Infantry Fighting Amphibious Modular Vehicle 1 31- 3...
 
Altus exertus-specification
Altus exertus-specificationAltus exertus-specification
Altus exertus-specification
 
Ching kuo (idf) multirole fighter jet, taiwan
Ching kuo (idf) multirole fighter jet, taiwanChing kuo (idf) multirole fighter jet, taiwan
Ching kuo (idf) multirole fighter jet, taiwan
 
AAV or EFV iteration 2nd Infantry Amphibious Modular Tank 33 - 38 t with 17 -...
AAV or EFV iteration 2nd Infantry Amphibious Modular Tank 33 - 38 t with 17 -...AAV or EFV iteration 2nd Infantry Amphibious Modular Tank 33 - 38 t with 17 -...
AAV or EFV iteration 2nd Infantry Amphibious Modular Tank 33 - 38 t with 17 -...
 
Aircraft
AircraftAircraft
Aircraft
 
Cn 235 persuader maritime patrol aircraft, spain
Cn 235 persuader maritime patrol aircraft, spainCn 235 persuader maritime patrol aircraft, spain
Cn 235 persuader maritime patrol aircraft, spain
 
Cutters And Aircraft
Cutters And AircraftCutters And Aircraft
Cutters And Aircraft
 
T129
T129T129
T129
 
DESIGN AND FABRICATION OF QUADCOPTER
DESIGN AND FABRICATION OF QUADCOPTERDESIGN AND FABRICATION OF QUADCOPTER
DESIGN AND FABRICATION OF QUADCOPTER
 
Helicopter Kamov-32
Helicopter Kamov-32 Helicopter Kamov-32
Helicopter Kamov-32
 

Recently uploaded

AI for Every Business: Unlocking Your Product's Universal Potential by VP of ...
AI for Every Business: Unlocking Your Product's Universal Potential by VP of ...AI for Every Business: Unlocking Your Product's Universal Potential by VP of ...
AI for Every Business: Unlocking Your Product's Universal Potential by VP of ...
Product School
 
FIDO Alliance Osaka Seminar: Passkeys at Amazon.pdf
FIDO Alliance Osaka Seminar: Passkeys at Amazon.pdfFIDO Alliance Osaka Seminar: Passkeys at Amazon.pdf
FIDO Alliance Osaka Seminar: Passkeys at Amazon.pdf
FIDO Alliance
 
Securing your Kubernetes cluster_ a step-by-step guide to success !
Securing your Kubernetes cluster_ a step-by-step guide to success !Securing your Kubernetes cluster_ a step-by-step guide to success !
Securing your Kubernetes cluster_ a step-by-step guide to success !
KatiaHIMEUR1
 
How world-class product teams are winning in the AI era by CEO and Founder, P...
How world-class product teams are winning in the AI era by CEO and Founder, P...How world-class product teams are winning in the AI era by CEO and Founder, P...
How world-class product teams are winning in the AI era by CEO and Founder, P...
Product School
 
GraphRAG is All You need? LLM & Knowledge Graph
GraphRAG is All You need? LLM & Knowledge GraphGraphRAG is All You need? LLM & Knowledge Graph
GraphRAG is All You need? LLM & Knowledge Graph
Guy Korland
 
The Future of Platform Engineering
The Future of Platform EngineeringThe Future of Platform Engineering
The Future of Platform Engineering
Jemma Hussein Allen
 
Builder.ai Founder Sachin Dev Duggal's Strategic Approach to Create an Innova...
Builder.ai Founder Sachin Dev Duggal's Strategic Approach to Create an Innova...Builder.ai Founder Sachin Dev Duggal's Strategic Approach to Create an Innova...
Builder.ai Founder Sachin Dev Duggal's Strategic Approach to Create an Innova...
Ramesh Iyer
 
UiPath Test Automation using UiPath Test Suite series, part 3
UiPath Test Automation using UiPath Test Suite series, part 3UiPath Test Automation using UiPath Test Suite series, part 3
UiPath Test Automation using UiPath Test Suite series, part 3
DianaGray10
 
Elevating Tactical DDD Patterns Through Object Calisthenics
Elevating Tactical DDD Patterns Through Object CalisthenicsElevating Tactical DDD Patterns Through Object Calisthenics
Elevating Tactical DDD Patterns Through Object Calisthenics
Dorra BARTAGUIZ
 
Epistemic Interaction - tuning interfaces to provide information for AI support
Epistemic Interaction - tuning interfaces to provide information for AI supportEpistemic Interaction - tuning interfaces to provide information for AI support
Epistemic Interaction - tuning interfaces to provide information for AI support
Alan Dix
 
FIDO Alliance Osaka Seminar: FIDO Security Aspects.pdf
FIDO Alliance Osaka Seminar: FIDO Security Aspects.pdfFIDO Alliance Osaka Seminar: FIDO Security Aspects.pdf
FIDO Alliance Osaka Seminar: FIDO Security Aspects.pdf
FIDO Alliance
 
Knowledge engineering: from people to machines and back
Knowledge engineering: from people to machines and backKnowledge engineering: from people to machines and back
Knowledge engineering: from people to machines and back
Elena Simperl
 
Assuring Contact Center Experiences for Your Customers With ThousandEyes
Assuring Contact Center Experiences for Your Customers With ThousandEyesAssuring Contact Center Experiences for Your Customers With ThousandEyes
Assuring Contact Center Experiences for Your Customers With ThousandEyes
ThousandEyes
 
Key Trends Shaping the Future of Infrastructure.pdf
Key Trends Shaping the Future of Infrastructure.pdfKey Trends Shaping the Future of Infrastructure.pdf
Key Trends Shaping the Future of Infrastructure.pdf
Cheryl Hung
 
DevOps and Testing slides at DASA Connect
DevOps and Testing slides at DASA ConnectDevOps and Testing slides at DASA Connect
DevOps and Testing slides at DASA Connect
Kari Kakkonen
 
State of ICS and IoT Cyber Threat Landscape Report 2024 preview
State of ICS and IoT Cyber Threat Landscape Report 2024 previewState of ICS and IoT Cyber Threat Landscape Report 2024 preview
State of ICS and IoT Cyber Threat Landscape Report 2024 preview
Prayukth K V
 
To Graph or Not to Graph Knowledge Graph Architectures and LLMs
To Graph or Not to Graph Knowledge Graph Architectures and LLMsTo Graph or Not to Graph Knowledge Graph Architectures and LLMs
To Graph or Not to Graph Knowledge Graph Architectures and LLMs
Paul Groth
 
FIDO Alliance Osaka Seminar: Overview.pdf
FIDO Alliance Osaka Seminar: Overview.pdfFIDO Alliance Osaka Seminar: Overview.pdf
FIDO Alliance Osaka Seminar: Overview.pdf
FIDO Alliance
 
Kubernetes & AI - Beauty and the Beast !?! @KCD Istanbul 2024
Kubernetes & AI - Beauty and the Beast !?! @KCD Istanbul 2024Kubernetes & AI - Beauty and the Beast !?! @KCD Istanbul 2024
Kubernetes & AI - Beauty and the Beast !?! @KCD Istanbul 2024
Tobias Schneck
 
Encryption in Microsoft 365 - ExpertsLive Netherlands 2024
Encryption in Microsoft 365 - ExpertsLive Netherlands 2024Encryption in Microsoft 365 - ExpertsLive Netherlands 2024
Encryption in Microsoft 365 - ExpertsLive Netherlands 2024
Albert Hoitingh
 

Recently uploaded (20)

AI for Every Business: Unlocking Your Product's Universal Potential by VP of ...
AI for Every Business: Unlocking Your Product's Universal Potential by VP of ...AI for Every Business: Unlocking Your Product's Universal Potential by VP of ...
AI for Every Business: Unlocking Your Product's Universal Potential by VP of ...
 
FIDO Alliance Osaka Seminar: Passkeys at Amazon.pdf
FIDO Alliance Osaka Seminar: Passkeys at Amazon.pdfFIDO Alliance Osaka Seminar: Passkeys at Amazon.pdf
FIDO Alliance Osaka Seminar: Passkeys at Amazon.pdf
 
Securing your Kubernetes cluster_ a step-by-step guide to success !
Securing your Kubernetes cluster_ a step-by-step guide to success !Securing your Kubernetes cluster_ a step-by-step guide to success !
Securing your Kubernetes cluster_ a step-by-step guide to success !
 
How world-class product teams are winning in the AI era by CEO and Founder, P...
How world-class product teams are winning in the AI era by CEO and Founder, P...How world-class product teams are winning in the AI era by CEO and Founder, P...
How world-class product teams are winning in the AI era by CEO and Founder, P...
 
GraphRAG is All You need? LLM & Knowledge Graph
GraphRAG is All You need? LLM & Knowledge GraphGraphRAG is All You need? LLM & Knowledge Graph
GraphRAG is All You need? LLM & Knowledge Graph
 
The Future of Platform Engineering
The Future of Platform EngineeringThe Future of Platform Engineering
The Future of Platform Engineering
 
Builder.ai Founder Sachin Dev Duggal's Strategic Approach to Create an Innova...
Builder.ai Founder Sachin Dev Duggal's Strategic Approach to Create an Innova...Builder.ai Founder Sachin Dev Duggal's Strategic Approach to Create an Innova...
Builder.ai Founder Sachin Dev Duggal's Strategic Approach to Create an Innova...
 
UiPath Test Automation using UiPath Test Suite series, part 3
UiPath Test Automation using UiPath Test Suite series, part 3UiPath Test Automation using UiPath Test Suite series, part 3
UiPath Test Automation using UiPath Test Suite series, part 3
 
Elevating Tactical DDD Patterns Through Object Calisthenics
Elevating Tactical DDD Patterns Through Object CalisthenicsElevating Tactical DDD Patterns Through Object Calisthenics
Elevating Tactical DDD Patterns Through Object Calisthenics
 
Epistemic Interaction - tuning interfaces to provide information for AI support
Epistemic Interaction - tuning interfaces to provide information for AI supportEpistemic Interaction - tuning interfaces to provide information for AI support
Epistemic Interaction - tuning interfaces to provide information for AI support
 
FIDO Alliance Osaka Seminar: FIDO Security Aspects.pdf
FIDO Alliance Osaka Seminar: FIDO Security Aspects.pdfFIDO Alliance Osaka Seminar: FIDO Security Aspects.pdf
FIDO Alliance Osaka Seminar: FIDO Security Aspects.pdf
 
Knowledge engineering: from people to machines and back
Knowledge engineering: from people to machines and backKnowledge engineering: from people to machines and back
Knowledge engineering: from people to machines and back
 
Assuring Contact Center Experiences for Your Customers With ThousandEyes
Assuring Contact Center Experiences for Your Customers With ThousandEyesAssuring Contact Center Experiences for Your Customers With ThousandEyes
Assuring Contact Center Experiences for Your Customers With ThousandEyes
 
Key Trends Shaping the Future of Infrastructure.pdf
Key Trends Shaping the Future of Infrastructure.pdfKey Trends Shaping the Future of Infrastructure.pdf
Key Trends Shaping the Future of Infrastructure.pdf
 
DevOps and Testing slides at DASA Connect
DevOps and Testing slides at DASA ConnectDevOps and Testing slides at DASA Connect
DevOps and Testing slides at DASA Connect
 
State of ICS and IoT Cyber Threat Landscape Report 2024 preview
State of ICS and IoT Cyber Threat Landscape Report 2024 previewState of ICS and IoT Cyber Threat Landscape Report 2024 preview
State of ICS and IoT Cyber Threat Landscape Report 2024 preview
 
To Graph or Not to Graph Knowledge Graph Architectures and LLMs
To Graph or Not to Graph Knowledge Graph Architectures and LLMsTo Graph or Not to Graph Knowledge Graph Architectures and LLMs
To Graph or Not to Graph Knowledge Graph Architectures and LLMs
 
FIDO Alliance Osaka Seminar: Overview.pdf
FIDO Alliance Osaka Seminar: Overview.pdfFIDO Alliance Osaka Seminar: Overview.pdf
FIDO Alliance Osaka Seminar: Overview.pdf
 
Kubernetes & AI - Beauty and the Beast !?! @KCD Istanbul 2024
Kubernetes & AI - Beauty and the Beast !?! @KCD Istanbul 2024Kubernetes & AI - Beauty and the Beast !?! @KCD Istanbul 2024
Kubernetes & AI - Beauty and the Beast !?! @KCD Istanbul 2024
 
Encryption in Microsoft 365 - ExpertsLive Netherlands 2024
Encryption in Microsoft 365 - ExpertsLive Netherlands 2024Encryption in Microsoft 365 - ExpertsLive Netherlands 2024
Encryption in Microsoft 365 - ExpertsLive Netherlands 2024
 

RUDAL.pptx

  • 1. CHINA RUSIA US PL-21  Mass : 270 kilogram (600 lb)  Length : 5,5 meter (18 kaki)  Diameter : 250–300 mm (9,8–11,8 in)  Warhead : 6kg blast-frag, or expanding rod (RF-fuse)  Detonation mechanism : Active infrared, laser proximity fuse(PL-5EII)  Engine : Ramjet  Wingspan 0.657m (PL-5B, PL-5C), 0.617m (PL-5E)  Operational range : 150 – 200 km  Speed Mach 2.5  Guidance Sistem : Actif radar with AESA  Launch platform : Aircraft,  Medium Range R-77  Mass : 175 kg (R-77), 190 kg (R-77-1)  Length : 3.6 m (R-77), 3.71 m (R-77-1)  Diameter : 200 mm  Warhead : 22.5 kg HE fragmenting (R-77)  Detonation mechanism Laser proximity fuse  Engine Solid fuel rocket motor (R-77), air- breathing ramjet (R-77-PD)  Wingspan700 mm  Operational range 80–100 km (R-77), 110 km (R-77-1), 193 km (R-77M)  Flight altitude : 5–25 km (16,000–82,000 ft)  Speed Mach 4, Mach 5 for K-77PD (RVV-AE- PD)  Guidance system : Inertial with mid-course update and terminal active radar homing/infrared homing (R-77T)  Launch platform : Aircraft:  Medium Range AIM 120-AMRAM  Mass : 335 lb (152 kg)  Length : 12 ft (3.7 m)  Diameter : 7 in (180 mm)  Warhead : High explosive blast-fragmentation  Detonation mechanism : Active RADAR Target Detection Device (TDD), Quadrant Target Detection Device (QTDD) in AIM-120C- 6 – lots 13+  Engine Solid-fuel rocket motor  Wingspan20.7 in (530 mm) AIM-120A/B  Operational range : AIM-120A/B: 55–75 km (30–40 nmi), AIM-120C-5: >105 km (>57 nmi), AIM-120D (C-8): >160 km (>86 nmi)[6]  Speed Mach : 4 (4,900 km/h; 3,045 mph)[citation needed  Guidance system : inertial guidance, terminal active radar homing  Launch platform : Aircraft:  Medium Range. AIR TO AIR MISSILE (MEDIUM RANGE)
  • 2. CHINA RUSIA US DF-12 M20  Type Short-range surface-to-air missile System  Country users : China  Warhead : 480 kg  System reaction time :10 sec.  Armament : Two missiles in individual container ready to fire  Range missile : Minimum 100 km; Maximum 280 km  Guidance system : Inertial guidance and INS with satellite guidance  Radar and command station : Command and control vehicle 9K720 ISKANDER-M/SS-26 STONE  Missile Variants : Iskander-M; Iskander-E (export)  Mobility and Role : Road-mobile; surface-to- surface short-range ballistic missile  Designer/Producer : Machine-Building Design Bureau  Range : 400-500 km (Iskander-M); 280 km (Iskander-E)  Warhead Type and Weight : Nuclear and conventional – 700 kg  Guidance System/Accuracy : Inertial and optical/10-30 m CEP (Iskander-M); Inertial/30-70 CEP (Iskander-E)  Stages/Propellant : One/Solid  IOC/Retirement : 2006 (Iskander-M)/Not Available Need updating by 2020 MGM-140 ATACMS  Mass : 3,690 pounds (1,670 kg)  Length : 13 feet (4.0 m)  Diameter : 24 inches (610 mm)  Maximum firing range: 190 mi (300 km)  Wingspan55 inches (1.4 m)  Flight ceiling : 160,000 ft (50 km)  Speed : In excess of Mach 3 (0.6 mi/s; 1.0 km/s)  Guidance System : GPS-aided inertial navigation guidance  Launch platform : M270, HIMARS. BALISTIC MISSILE (TACTICAL MISSILE)
  • 3. CHINA RUSIA US DF-11  Type : SRBM (Short Range Balistic Missile)  Used by PRC  Production history  Manufacturer :Academy of Rocket Motors Technology  Specifications  Mass 3,800 kg[1]  Length 7.5-8.5 m[2]  Diameter 0.86 m  Warhead 500 kg: 2/10/20 kiloton nuclear warhead, fuel-air explosive (FAE), chemical, or submunition  Engine single-stage solid-propellant rocket  Operational range : DF-11:300+ km  DF-11A:700+ km, DF-11AZT:600 km  Guidance System :Astro-inertial guidance (including ring-laser gyroscope) + Beidou  Launch Platform : Road-mobile TEL P-800 ONIKS (SS-N-26)  Russian/NATO Designation P-800 Oniks (Land- based Yakhont)/SS-N-26 Strobile Variants BrahMos  Mobility and Role :  Surface-to-Surface Anti-Ship Cruise Missile  Max Speed 3000 km/h  Designer/Producer NPO Mashinostroyeniya  Range 300km  Warhead Type and Weight  3000kg launch weight  HE warhead; Armor-Piercing Warhead Yield  200kg HE warhead;  250 kg Armor-piercing warhead  Guidance System/Accuracy  1.5m CEP  Satellite Guidance; Active Radar Seeker  Cruise Altitude Max 14,000 m  Propellant Solid-fuel Booster; Liquid-Fuel Ramjet Sustainer  IOC/Retirement :2002/Operational  Status/Number of Units Operational/Unknown  Launch Vehicles  Nakat class missile ship; Yasen class submarine;  Bastion-P/Bastion-S ground-launch system PGM-11 REDSTONE BALISTIC MISSILE (SHORT RANGE)  Mass : 61,207 pounds (27,763 kg) at ignition  Length : 69.3 feet (21.1 m)  Diameter : 5.83 feet (1.8 m)  Blast yield :3.5 megatons of TNT (15 PJ) or 500 kilotonnes of TNT (2.1 PJ)  thermonuclear warhead  Engine : Rocketdyne North American Aviation 75–110 A-7  78,000 pounds-force (350 kN) thrust at sea level for 121 seconds  Payload capacity : 6,305 pounds (2,860 kg)  Propellant ethyl alcohol, liquid oxygen, hydrogen peroxide  Fuel capacity : alcohol: 11,135 pounds (5,051 kg), liquid oxygen: 25,280 pounds (11,470 kg), hydrogen peroxide: 790 pounds (360 kg)  Operational range : 57.5 miles (92.5 km) to 201 miles (323 km)  Flight altitude : 28.4 miles (45.7 km) peak minimum to 58.7 miles (94.5 km) peak maximum  Boost time: 97 seconds to 117 seconds  Speed Mach : 5.5 maximum at re-entry interface  Guidance System : Ford Instrument Company ST-80 inertial guidance  Steering System : Carbon jet vanes, air rudders, spatial air jet nozzles, air vanes  Accuracy : 300 metres (980 ft) CEP  Launch platform :Guided missile platform launcher M74
  • 4. CHINA RUSIA US DF-21 - Mass 14,700 kilograms (32,400 lb) - Length 10.7 metres (35 ft) - Diameter 1.4 metres (4.6 ft) - Warhead 600kg: 1, or 5-6 (improved variant)[1] 200-300-500 kt nuclear[2] - Engine Solid fueled - Operational range :1,770 km (1,100 mi) (DF- 21/DF-21A), 1,700 km (1,100 mi) (DF-21C) - 1,500 km (930 mi; 810 nmi) (DF-21D ASBM)[4] - Speed Mach : 10 - Guidance System:Inertial + terminal active radar guidance - Accuracy :DF-21 700m, DF-21A 50m, DF-21B 10m CEP (with BeiDou Navigation Satellite System and active radar) - Launch Platform : Mobile launcher SSC - 8  Country of origin : Russia  Entered service : 2018  Crew : 3 men  Number of missiles : 4  Weight : ~ 40 t  Length : 13.25 m  Width : 3.51 m  Height : 3.94 m  Missile length (including booster) : ~ 8 m  Missile diameter : 0.53 m  Wing span : ~ 3 m  Missile weight : ~ 2 300 kg  Warhead weight : 400 ~ 500 kg  Warhead type : Nuclear  Range : 2 000 ~ 2 500 (?)  CEP : ~ 5 m Mobility :  Engine : YaMZ-846 diesel  Engine power : 500 hp  Maximum road speed :70 km/h  Range : 1 000 km – 5000 Km  Maneuverability  Gradient :45%  Side slope : 30%  Vertical step : ~ 0.6 m  Trench : 2 m  Fording : 1.4 m AGM-86  Overall length: 19.82 m (65.0 ft)  Span: 2.74 m (9.0 ft)  Weight: 49,800 kg (109,800 lb)  Empty weight: 3,125 kg (6,889 lb)  Core Diameter: 2.44 m  Maximum range: 2,400 km (1,500 mi)  Ceiling: 480 km (300 mi)  Guidance: Inertial  Maximum speed: 17,740 km/h (11,020 mph)  Engines: Vernier: 2x Rocketdyne LR101-NA; 4.5 kN (1000 lbf)  Warhead : One W49 warhead on Mk. 2 reentry vehicleMass 3,150 pounds (1,430 kg)  Length 20 ft. 9 in. (6.3 m)  Diameter 24.5 inches (620 mm)[  Warhead W80 thermonuclear weapon (AGM-86B)  conventional warhead (AGM-86C)  AUP warhead (AGM-86D)  Warhead weight : 908kg (AGM-86C Block 0)  1362kg (AGM-86C Block 1)  1,200 lb class advanced unitary penetrating warhead (AGM-86D)  Engine : Williams International  F107-WR-101 turbofan engine  600 lbf (2.7 kN) thrust  Wingspan 12 feet (3.7 m)  Guidance system : AGM-86B: Litton inertial nav system element with TERCOM, AGM 86C: Litton INS element integrated with GPS  Launch platform : Boeing B-52H Stratofortress BALISTIC MISSILE (MEDIUM RANGE)
  • 5. CHINA RUSIA US JL-2  Type : SLBM (Submarine Launched Balistic Missile)  Place of origin :People's Republic of China  Service history  In service Active as of 2015  Used by People's Liberation Army Navy  Specifications  Mass : 42,000 kilograms (93,000 lb)[2]  Length : 13 metres (43 ft)[2]  Warhead : 1 nuclear warhead[3]  Blast yield : 1 megaton of TNT (4.2 PJ)[4]  Propellant : Solid-fuel rocket  Operational Range : 7,200 km (4,500 mi)[5]  Guidance System : Astro-inertial[4] with Beidou  Launch Platform : Type 094 submarine SS-19 STILLETO  Length (m) : 17.2  Body diameter (m) : 2.5  Fueled weight (t) : 86.3  Engine Designation : RD-0233 / RD-0234,  RD-0235 (14/15D113)  Vernier Engine Designation RD-0236 (15D114)  Bus Engine Designation Third Stage RD-0237  Fuel : UDMH  Oxidizer : Nitrogen Tetroxide  Payload (t) : 4.350  Total length (m) : 24.3  Warhead (m) : 21.1  Missile Diameter (m) : 2.50  Launch Weight (t) : 103.4 - 105.6  Fuel Weight (t) : 93.1  Range (km) : 10,000 MINUTEMAN III  Berat : 78,000 lb (35,300 kg)  Panjang : 59 ft 9.5 in (18.2 m)  Diameter : 5 ft 6 in (1.7 m) (1st stage)  Hulu ledak : Nuclear W62, W78, or (2006-) W87  Jenis Mesin : Three solid-propellant rocket motors; first stage - Thiokol TU-122 (M-55); second stage - Aerojet-General SR-19-AJ-1; third stage - Aerojet/Thiokol SR73-AJ/TC-1  Daya jelajah : 8,100 miles (13,000 km)  Ketinggian terbang : 700 miles (1,120 kilometers)  Kecepatan Approximately : 15,000 mph (Mach 23, or 24,100 km/h, or 7 km/s) (terminal phase)  Sistem penuntun : Inertial  Alat Peluncur : Silo BALISTIC MISSILE (LONG RANGE)
  • 6. CHINA RUSIA US QW-2 VANGUARD 2  Type MANPAD  Service history 1990’s to present  Used by China and Bangladesh  Production history  Produced : Since Mid 1990’s Specifications  Weight : 11.32 kg, 18 kg with launcher  Length : 1.59 meter  Detonation  mechanism : Impact & Proximity  Engine rocket  Propellant : solid rocket  Operational Range : 6 km maximum  Flight ceiling : 3 km  Flight altitude : 10 meter minimum  Speed > 600 m/s  Guidance System : Infrared homing  Launch Platform : MANPADS, Type 95 SPAAA PANTSIR (S1, S2 & S3)  Armament : Twelve ground-to-air missile launcher 57E6 / 57E6-E, two dual 2A38M 30 mm autocannon guns  Country users : Iran, Iraq, Serbia, United Arab Emirates, Jordan, Russia, Syria, Vietnam  Designer Company : KBP Instrument Design Bureau  Accessories : Radio commands with IR or radio direction finding, autonomous acquisition radar and tracking radar  Crew : 3 soldiers  Radar System : Autonomous acquisition and tracking radar 1RS2-1  Range missile : 1 – 30 km  Weight missile : 90 kg with container MIM-104 PATRIOT (PAC3)  Specifications (PAC-1)  Mass : 700 kg (1,500 lb)  Length : 5,800 mm (19 ft 0 in)  Diameter : 410 mm (16 in)  Warhead : M248 Composition B HE blast/ fragmentation with two layers of pre-formed fragments and Octol 75/25 HE blast/ fragmentation  Warhead weight : 200 lb (90 kg)  Detonation mechanism : Proximity fuze  Wingspan : 920 mm (3 ft 0 in)  Propellant : Solid-fuel rocket  Operational Range : PAC-3: 20 km against ballistic missile, PAC-3 MSE: 35 km against ballistic missile  Flight altitude : 79,500 feet (24,200 m)  Speed : PAC-1: Mach 2.8, PAC-2/PAC-3: Mach 4.1  Guidance System : PAC-1: Radio command with Track Via Missile semi-active homing, PAC-3: Ka Band AESA seeker  Launch Platform : Mobile trainable four-round semi-trailer SURFACE TO AIR MISSILE (SHORT RANGE)
  • 7. CHINA RUSIA US KS-1  Weight: 900 kg  Warhead: > 100 kg  Length: 5.6 m  Diameter: 0.4 m  Speed: 1,200 m/s  Maneuverability: > 20 g  Maximum target speed: 750 m/s  Maximum target maneuverability: > 5 g  Maximum range: > 50 km  Minimum range: 100 m  Maximum altitude: > 25 km  Minimum altitude: < 500 m S-300 VM  Operational Range : 200 (250) km against MRBMs  9M82M missile  Type : Surface-to-air missile  Place of origin : Russia  Production history  Designer : Almaz-Antey  Designed 2000s  Manufacturer : Almaz-Antey  Produced : 2013-present  Variants 9M82M, 9M83M  Specifications (9M82M  Operational Range : 200 kilometres (120 mi)  Flight altitude : 30,000 metres (98,000 ft) MIM-104 PATRIOT (PAC1 & PAC2)  Specifications (PAC-1)  Mass : 700 kg (1,500 lb)  Length : 5,800 mm (19 ft 0 in)  Diameter : 410 mm (16 in)  Warhead : M248 Composition B HE blast/ fragmentation with two layers of pre-formed fragments and Octol 75/25 HE blast/ fragmentation  Warhead weight : 200 lb (90 kg)  Detonation mechanism : Proximity fuze  Wingspan : 920 mm (3 ft 0 in)  Propellant : Solid-fuel rocket  Operational Range : PAC-1: 70 km  PAC-2: 96 km-160 km  Flight altitude : 79,500 feet (24,200 m)  Speed : PAC-1: Mach 2.8, PAC-2/PAC-3: Mach 4.1  Guidance System : PAC-1: Radio command with Track Via Missile semi-active homing, PAC-3: Ka Band AESA seeker  Launch Platform : Mobile trainable four-round semi-trailer SURFACE TO AIR MISSILE (MEDIUM RANGE)
  • 8. CHINA RUSIA US HG-9  Mass :1300 kg  Length : 6.8 m  Warhead weight :180 kg  Engine Two-stage solid propellant rocket  Operational Range : 200 km (FD-2000 version) 250 km (HQ-9A version) 300+ km for HQ-9B version  Flight ceiling : 27 km, 41 km for HQ-9B  Speed Mach : 4.2  Guidance System Inertial guidance with mid- course update and terminal active radar homing  Launch Platform : Taian TA580/TAS5380 8×8 transporter erector launcher (TEL)  Type 052C destroyer  Type 052D destroyer  Type 055 destroy S-500 PROMETHEUS  S-500 launcher based on the BAZ-69069 chassis  Country of origin : Russia  Entered service : Expected in 2025  Crew 3 men  Weight 54 t  Length ~ 14.5 m  Width ~ 3 m  Range of fire : 500 ~ 600 km  Altitude of fire : ~ 40 km  Mobility :  Engine : diesel  Engine power : 550 hp  Maximum road speed ~ 70 km/h  Range ~ 1 000 km  Maneuverability  Gradient 60%  Side slope 30%  Vertical step ~ 0.6 m  Trench ~ 2 m  Fording 1.7 m; AN/TWQ-1 AVENGER  Country of origin : United States  Entered service : 1990  Crew : 2 men  Weight 4.3 t  Length 4.95 m  Width 2.49 m  Height 2.64 m  Missile length 1.52 m  Missile diameter 0.07 m  Missile weight 10.1 kg  Warhead weight 3 kg  Warhead type HE-FRAG  Range of fire 4 - 8 km  Altitude 3.5 - 3.8 km  Guidance : Infrared homing  Engine Detroit Diesel diesel  Engine power 135 hp  Maximum road speed 100 km/h  Range 480 km  Maneuverability  Gradient 60%  Side slope : 30%  Vertical step : 0.5 m  Trench : 0.5 m  Fording : 0.75 - 1.5 m SURFACE TO AIR MISSILE (LONG RANGE)
  • 9. CHINA RUSIA US YJ-12B  Country of origin China  Crew ~ 5  Weight ~ 40 t  Length ~ 16 m  Width ~ 3 m  Height ~ 3.5 m  Warhead weight 200 kg  Warhead type HE-FRAG  Range of fire 400 ~ 500 km  Guidance : Inertial with active radar homing  Mobility  Engine Deutz diesel  Engine power : 544 hp  Maximum road speed :70 km/h  Range 650 km  Maneuverability  Gradient 40%  Side slope : 20%  Vertical step : 0.4 m  Trench 2.5 m  Fording 1.2 m BAL  Country of origin Russia  Entered service 2004  Crew 3 men  Weight ~ 40 t  Length ~ 12.8 m  Width ~ 3 m  Height ~ 3.6 m  Missile length 4.4 m  Missile diameter 0.42 m  Wing span 1.33 m  Missile weight 620 - 670 kg  Warhead weight 145 kg  Warhead type HE-FRAG  Range of fire 130 / 260 km  Engine YaMZ-846  Engine power 500 hp  Maximum road speed 70 km/h  Range 1 000 km  Maneuverability Gradient 45%  Side slope 30%  Vertical step ~ 0.6 m  Trench 2 m  Fording 1.4 m BGM-109G GRYPHON  Country of origin United States  Entered service 1983  Crew 3 men  Number of missiles 4  Weight 36 t  Length 19.8 m  Width 2.44 m  Height ~ 3 m  Missile length (without booster) 5.56 m  Missile diameter 0.52 m  Missile launch weight 1 200 kg  Warhead weight 176 kg  Warhead type Nuclear, 150 kT yield  Range of fire 2 500 km  CEP ~ 30 m  Engine MAN D2866 KFG diesel  Engine power 360 hp  Maximum road speed 80 - 90 km/h  Range ~ 800 km  Maneuverability  Gradient (with trailer) ~ 20%  Fording ~ 1.2 m COASTAL DEFENSE SYSTEM (ANTI SHIP MISSILE)