The document provides specifications for various air-to-air and surface-to-air missiles from China, Russia, and the US. It includes details on mass, length, diameter, warhead, engine, range, guidance system, and launch platform for missiles like the PL-21, R-77, AIM-120, DF-12, Iskander-M, ATACMS, DF-11, P-800 Oniks, Redstone, DF-21, SSC-8, AGM-86, JL-2, Minuteman III, and QW-2 Vanguard 2. The missiles covered span short, medium and long ranges and include air-to-air,
Fighter jet design and performance calculations by using the case studies.Mani5436
1.Fighter jet theoretical calculations by using previous calculations.
2. Case study of the fighter jet
3. Configuration selection of the fighter jet
4. Aircraft Performance
Fighter jet design and performance calculations by using the case studies.Mani5436
1.Fighter jet theoretical calculations by using previous calculations.
2. Case study of the fighter jet
3. Configuration selection of the fighter jet
4. Aircraft Performance
Mission Definition:
Ÿ Flight demonstration and evaluation of Test Vehicle sub systems.
Ÿ Flight demonstration and evaluation of Crew Escape System including various
separation systems.
Ÿ Crew Module characteristics & deceleration systems demonstration at higher
altitude & its recovery
The T129 is a formidable, new, highly powerful and capable all-weather day and night multi-role attack helicopter which is being developed in cooperation by AgustaWestland, Aselsan and TAI (Turkish Aerospace Industries) for Turkey and other export markets.
Mission Definition:
Ÿ Flight demonstration and evaluation of Test Vehicle sub systems.
Ÿ Flight demonstration and evaluation of Crew Escape System including various
separation systems.
Ÿ Crew Module characteristics & deceleration systems demonstration at higher
altitude & its recovery
The T129 is a formidable, new, highly powerful and capable all-weather day and night multi-role attack helicopter which is being developed in cooperation by AgustaWestland, Aselsan and TAI (Turkish Aerospace Industries) for Turkey and other export markets.
Securing your Kubernetes cluster_ a step-by-step guide to success !KatiaHIMEUR1
Today, after several years of existence, an extremely active community and an ultra-dynamic ecosystem, Kubernetes has established itself as the de facto standard in container orchestration. Thanks to a wide range of managed services, it has never been so easy to set up a ready-to-use Kubernetes cluster.
However, this ease of use means that the subject of security in Kubernetes is often left for later, or even neglected. This exposes companies to significant risks.
In this talk, I'll show you step-by-step how to secure your Kubernetes cluster for greater peace of mind and reliability.
GraphRAG is All You need? LLM & Knowledge GraphGuy Korland
Guy Korland, CEO and Co-founder of FalkorDB, will review two articles on the integration of language models with knowledge graphs.
1. Unifying Large Language Models and Knowledge Graphs: A Roadmap.
https://arxiv.org/abs/2306.08302
2. Microsoft Research's GraphRAG paper and a review paper on various uses of knowledge graphs:
https://www.microsoft.com/en-us/research/blog/graphrag-unlocking-llm-discovery-on-narrative-private-data/
Builder.ai Founder Sachin Dev Duggal's Strategic Approach to Create an Innova...Ramesh Iyer
In today's fast-changing business world, Companies that adapt and embrace new ideas often need help to keep up with the competition. However, fostering a culture of innovation takes much work. It takes vision, leadership and willingness to take risks in the right proportion. Sachin Dev Duggal, co-founder of Builder.ai, has perfected the art of this balance, creating a company culture where creativity and growth are nurtured at each stage.
UiPath Test Automation using UiPath Test Suite series, part 3DianaGray10
Welcome to UiPath Test Automation using UiPath Test Suite series part 3. In this session, we will cover desktop automation along with UI automation.
Topics covered:
UI automation Introduction,
UI automation Sample
Desktop automation flow
Pradeep Chinnala, Senior Consultant Automation Developer @WonderBotz and UiPath MVP
Deepak Rai, Automation Practice Lead, Boundaryless Group and UiPath MVP
Elevating Tactical DDD Patterns Through Object CalisthenicsDorra BARTAGUIZ
After immersing yourself in the blue book and its red counterpart, attending DDD-focused conferences, and applying tactical patterns, you're left with a crucial question: How do I ensure my design is effective? Tactical patterns within Domain-Driven Design (DDD) serve as guiding principles for creating clear and manageable domain models. However, achieving success with these patterns requires additional guidance. Interestingly, we've observed that a set of constraints initially designed for training purposes remarkably aligns with effective pattern implementation, offering a more ‘mechanical’ approach. Let's explore together how Object Calisthenics can elevate the design of your tactical DDD patterns, offering concrete help for those venturing into DDD for the first time!
Epistemic Interaction - tuning interfaces to provide information for AI supportAlan Dix
Paper presented at SYNERGY workshop at AVI 2024, Genoa, Italy. 3rd June 2024
https://alandix.com/academic/papers/synergy2024-epistemic/
As machine learning integrates deeper into human-computer interactions, the concept of epistemic interaction emerges, aiming to refine these interactions to enhance system adaptability. This approach encourages minor, intentional adjustments in user behaviour to enrich the data available for system learning. This paper introduces epistemic interaction within the context of human-system communication, illustrating how deliberate interaction design can improve system understanding and adaptation. Through concrete examples, we demonstrate the potential of epistemic interaction to significantly advance human-computer interaction by leveraging intuitive human communication strategies to inform system design and functionality, offering a novel pathway for enriching user-system engagements.
Key Trends Shaping the Future of Infrastructure.pdfCheryl Hung
Keynote at DIGIT West Expo, Glasgow on 29 May 2024.
Cheryl Hung, ochery.com
Sr Director, Infrastructure Ecosystem, Arm.
The key trends across hardware, cloud and open-source; exploring how these areas are likely to mature and develop over the short and long-term, and then considering how organisations can position themselves to adapt and thrive.
DevOps and Testing slides at DASA ConnectKari Kakkonen
My and Rik Marselis slides at 30.5.2024 DASA Connect conference. We discuss about what is testing, then what is agile testing and finally what is Testing in DevOps. Finally we had lovely workshop with the participants trying to find out different ways to think about quality and testing in different parts of the DevOps infinity loop.
State of ICS and IoT Cyber Threat Landscape Report 2024 previewPrayukth K V
The IoT and OT threat landscape report has been prepared by the Threat Research Team at Sectrio using data from Sectrio, cyber threat intelligence farming facilities spread across over 85 cities around the world. In addition, Sectrio also runs AI-based advanced threat and payload engagement facilities that serve as sinks to attract and engage sophisticated threat actors, and newer malware including new variants and latent threats that are at an earlier stage of development.
The latest edition of the OT/ICS and IoT security Threat Landscape Report 2024 also covers:
State of global ICS asset and network exposure
Sectoral targets and attacks as well as the cost of ransom
Global APT activity, AI usage, actor and tactic profiles, and implications
Rise in volumes of AI-powered cyberattacks
Major cyber events in 2024
Malware and malicious payload trends
Cyberattack types and targets
Vulnerability exploit attempts on CVEs
Attacks on counties – USA
Expansion of bot farms – how, where, and why
In-depth analysis of the cyber threat landscape across North America, South America, Europe, APAC, and the Middle East
Why are attacks on smart factories rising?
Cyber risk predictions
Axis of attacks – Europe
Systemic attacks in the Middle East
Download the full report from here:
https://sectrio.com/resources/ot-threat-landscape-reports/sectrio-releases-ot-ics-and-iot-security-threat-landscape-report-2024/
Kubernetes & AI - Beauty and the Beast !?! @KCD Istanbul 2024Tobias Schneck
As AI technology is pushing into IT I was wondering myself, as an “infrastructure container kubernetes guy”, how get this fancy AI technology get managed from an infrastructure operational view? Is it possible to apply our lovely cloud native principals as well? What benefit’s both technologies could bring to each other?
Let me take this questions and provide you a short journey through existing deployment models and use cases for AI software. On practical examples, we discuss what cloud/on-premise strategy we may need for applying it to our own infrastructure to get it to work from an enterprise perspective. I want to give an overview about infrastructure requirements and technologies, what could be beneficial or limiting your AI use cases in an enterprise environment. An interactive Demo will give you some insides, what approaches I got already working for real.
Encryption in Microsoft 365 - ExpertsLive Netherlands 2024Albert Hoitingh
In this session I delve into the encryption technology used in Microsoft 365 and Microsoft Purview. Including the concepts of Customer Key and Double Key Encryption.
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)