In today’s Prelims 20+, we focus on Space Technology and Defence—critical pillars of India’s strategic and technological landscape. From cutting-edge satellite missions and indigenous launch capabilities to breakthroughs in missile systems and defence manufacturing, this area reflects India’s growing self-reliance and geopolitical aspirations. It holds immense relevance for the UPSC Civil Services Examination, particularly in understanding national security, innovation, and international collaborations.
Space Tech
Rocket Engines
- Rocket engines operate on the principle of Newton’s third law of motion: for every action, there is an equal and opposite reaction. In a rocket engine, a propellant (fuel and oxidizer) is ignited in a combustion chamber.
- This combustion produces high-pressure gases that are expelled through a nozzle at high velocity. The force of these gases rushing out of the nozzle creates thrust, propelling the rocket forward.
Rocket Fuels
| Aspect | Solid Rocket Fuel | Liquid Rocket Fuel |
| Composition | Fuel and oxidizer mixed and bound in solid form | Separate liquid fuel and oxidizer |
| Storage | Stored as a single solid block | Stored in separate insulated tanks |
| Ignition | Simple and immediate upon ignition | Requires complex ignition systems |
| Throttling | Non-throttleable, burns until exhausted | Throttleable, can control thrust output |
| Complexity | Simple design, easier to manufacture and handle | Complex design, involves pumps and plumbing |
| Efficiency | Generally less efficient | Higher efficiency, better specific impulse |
| Usage | Used for boosters and short-duration missions | Used for main engines and long-duration missions |
| Examples of Use | Space Shuttle Solid Rocket Boosters, Fireworks | Saturn V, SpaceX Falcon 9, Ariane 5 |
| Advantages | Simple, reliable, lower cost | Controllable, higher performance |
| Disadvantages | Cannot be shut down once ignited, less efficient | Complex, expensive, handling/storage challenges |
| Examples of fuels | Ammonium perchlorate composite propellant (APCP), Black powder, Zinc-sulfur | Liquid Hydrogen (LH2) with Liquid Oxygen (LOX), RP-1 (refined kerosene) with LOX, Hypergolics like Hydrazine (N2H4) with Nitrogen Tetroxide (N2O4) |
Cryogenic Engines
- Uses propellants that are gases at room temperature but are cooled to cryogenic temperatures to become liquids. Common propellants include liquid hydrogen (LH2) and liquid oxygen (LOX).
- Liquid hydrogen and liquid oxygen mix and burn, creating a high-temperature, high-pressure exhaust gas.
- The exhaust gases are expelled through a nozzle, converting thermal energy into kinetic energy.
Comparison with Conventional Engines
| Feature | Conventional Engines (Solid/Liquid Non-Cryogenic) | Cryogenic Engines |
| Specific Impulse | Lower | Higher |
| Thrust | Moderate | Higher |
| Combustion Byproducts | CO2, H2O (if hydrocarbon fuels) | Mostly H2O (cleaner) |
| Fuel State | Solid or liquid at room temperature | Liquid at cryogenic temperatures |
| Efficiency | Lower | Higher |
| Complexity | Simple to moderate | High (due to cryogenic handling) |
| Use Cases | Boosters, short-duration missions | Upper stages, deep-space missions, heavy lift |
Satellite
- A satellite orbits a planet or a star.
- Two types – natural (moon) and human-made/artificial (machine);
- Artificial satellite: machine launched into space which moves around the around earth or other object.
- Application: weather forecasting, study of planets and galaxies, in communication and information technology, GPS.
Satellite Orbits
- It is a repeating path that one object in space takes around another one.
- Orbits- inclination angle
- It is the angle between the plane of an orbit and the equator.
- An orbital inclination of 0° is directly above the equator; 90° crosses right above the pole, and 180° orbits above the equator in the opposite direction of Earth’s spin.
Types of satellite orbits
- `Satellites orbit around the earth in different planes – equatorial orbit (orbit directly above the earth’s equator); polar orbit (orbit that passes over both the poles.)
- Other orbits are inclined; Orbits maybe circular or elliptical.
- Altitude of communication can be GEO (geostationary earth orbit), MEO (medium earth orbit), LEO (low earth orbit).
- Polar orbit
- An orbit in which a satellite passes above Earth’s North and South poles on each revolution.
- Has an inclination of 90 degrees to the equator.
- Sun-synchronous orbit (SSO)
- Satellites in SSO, travelling over the Polar Regions, are synchronous with the Sun.
- They are synchronized to be at a fixed position relative to the sun which enables the satellite to always visit the same spot at the same local time.
- LEO (low earth orbit)- Polar orbit: altitude of 50-1500km and orbital period range (95-120 minutes)
- MEO (medium earth orbit)
- Positioned somewhere between LEO and GEO altitude of 5000-12000kminclination towards equatorial plane.; Orbital period of satellite 6hrs; Medium propagation delay
- Cover large arearequires less handover; Provides true global coverage.
- Requires large number of satellites for coverage Long time to deploy a full constellation.
- GEO (geostationary earth orbit)
- Geosynchronous orbit- Orbital period of earth (24 Hours); altitude of 35,863 km above earth’s surface;
- Geostationary orbit- Inclination of the orbit are zero; appears stationary from earth
- Disadvantage- large propagation delay; affects voice and time data protocol; high launch cost.
- GTO (geosynchronous transfer orbit)
- Elliptical orbit, with an apogee of 35,784km
- Inclination equal to the latitude of the launch site, into which a spacecraft is initially placed before being transferred to a geosynchronous/ geostationary orbit.
Satellite Launch vehicle
- Rocket powered vehicle used to transport any spacecraft into earth’s atmosphere.
- Used to send various satellites, spacecrafts and space probes into space.
- India’s used launch vehicle- RLV-TD, SLV, ASLV, PSLV, GSLV.

Satellite launch vehicle (SLV) and augmented satellite launch vehicle (ASLV)
| Satellite launch vehicle | Augmented launch vehicle |
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PSLV (polar satellite launch vehicle): third generation
- Most reliable and popular launch vehicle in service for over 20 years; First Indian launch vehicle to have liquid stages;
- Payload: PSLV can take up to 1,750 kg of payload to Sun-Synchronous Polar Orbits of 600 km altitude and up to 1425kg to geostationary orbits.
- Has a four stage multi propellant launcher that has a height of 44 meters and a lift off 320 tons (PSLV XL).
| First stage (SOLID) PS1 |
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| Second stage (LIQUID) PS2 |
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| Third Stage(SOLID) PS3 |
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| Fourth Stage (LIQUID) PS4 |
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Note – Chandrayaan-1 in 2008 and Mars Orbiter Spacecraft in 2013 were launched through PSLV-XL (most remarkable mission of ISRO).
Geosynchronous satellite launch vehicle (GSLV): fourth generation
- Developed to launch geosynchronous satellites into geostationary orbit.
- 3 stage launch vehicle, first two stages are similar to PSLV with same solid and liquid natures of fuel; third stage is cryogenic stage.
- Three variants include:
- GSLV Mark I (a) ( capability of 1500 kg’s)
- GSLV Mark I (b) (capability of 1900 kg’s )
- GSLV M ark II (uses Indian cryogenic engine and is capable of launching 2,500 kg’s of payload to geostationary orbit and up to 5000 kg’s of payload to LEO.)
| First Stage GS1 (SOLID) |
| It is derived from the PSLV’s first stage (PS1). This stage uses Hydroxyl-terminated polybutadiene (HTPB) as its fuel. The four liquid engine strap-ons for extra thrust. |
| Second Stage GS2 (LIQUID) |
| This stage was derived from the second stage (PS2) of PSLV using the Vikas engine. It uses Unsymmetrical dimethylhydrazine (UDMH) as fuel and dinitrogen tetroxide (N2O4) as oxidiser. |
| Third stage GS3 CUS (CRYOGENIC) |
| Third Stage is the Cryogenic Upper Stage and it uses liquid oxygen and liquid hydrogen as its fuel. |
- GSLV MK-III
- Three -stage heavy lift launch vehicle.
- Intended for carrying 4 ton class of satellites into geosynchronous transfer orbit (GTO) or about 10 tons to low earth orbit (LEO), which being the double the GSLV Mk II capacity.
- GSLV Mk III-M1, successfully injected Chandrayaan-2, CARE mission (crew module atmospheric re-entry experiment.), India’s second lunar mission, into earth parking orbit.
- Will be used to launch Gaganyaan mission.
Ariane -5
- European heavy-lift launch vehicle that can carry payloads weighing more than 10 metric tons to GTO and over 20 metric tons into low-earth orbit (LEO).
Types of Satellite
- Earth Observation
- Satellite imaging and remote sensing – spectral fingerprint;
- Most orbit at altitudes above 500 to 600 kilometres; Orbits have significant air-drag;
- Remote sensing – acquisition of information without making physical contact; Active or Passive;
- Types
- Passive – studying reflected light e.g. IR, Radiometers;
- Active – RADAR & LIDAR;
- Synthetic aperture radars; multi-spectral imaging; Hyperspectral imaging (vast portion of the electromagnetic spectrum. continuous scan); Acoustic – Ultrasound – water levels;
Communication Satellite
- Relays and amplifies radio signals via a transponder;
- Orbit – largely Geosynchronous, geostationary;
- Uses: television, telephone, radio, internet, and military applications
- Frequency ranges or “bands” – minimize interference; Assigned by ITU; E.g. C-band 4-8 Ghz, KU band- 12-18 GHz, KA band;
- E.g. INSAT, GSAT;
Telescopes
| Frequency | Characteristics | Examples | Advantages | Challenges |
| Infrared | Detects heat, sees through dust clouds | Spitzer,Herschel | Observes cool objects, sees through dust | Requires cooling, atmospheric absorption |
| Ultraviolet | Observes hot stars, quasars, interstellar medium | Hubble, Galex | Studies young stars, active galaxies | Absorbed by atmosphere, needs space-based observatories |
| X-ray | Studies high-energy processes | Chandra, XMM-Newton | Observes black holes, neutron stars, hot gas | Absorbed by atmosphere, requires advanced technology |
| Gamma-ray | Detects highest energy events | Fermi, Compton | Studies gamma-ray bursts, AGNs, supernovae | Absorbed by atmosphere, needs specialized instruments |
Ground Telescopes
- GMRT (PUNE): Giant Meterwave Radio Telescope: Array of 30 fully steerable radio telescopes
- Thirty Meter Telescope: Multi wavelength; near-UV to mid-infra; Mauna Kea (Hawaii) or Hanle (India)
- Meerkat: South Africa; Largest telescope in Southern Hemisphere;
Navigation
- IRNSS
- Objective: provide reliable position, navigation and timing services over India and its neighborhood;
- India became one of the 5 countries having their own navigation system like GPS of USA, GLONASS of Russia, Galileo of Europe and BeiDou of China
- Constellation: Consists of eight satellites, 3 in geostationary and 5 satellites in geosynchronous.
- Range: India + 1,500-km radius over the sub-continent;
- Satellites: The satellites are named as- IRNSS – 1A, 1B, 1C, 1D, 1E, 1F, 1G. (3 Geostationary, 4 Geosynchronous)
- Services:
- Standard positioning service: open for civilian use and
- Restricted service: encrypted for authorised users like military
- Applications: Terrestrial, aerial and marine navigation; Disaster management; Vehicle tracking and fleet management; Integration with mobile phones; Precise timing (as for ATMs and power grids);
- Working of GPS
- Global Positioning System (GPS) is a US based navigation system.
- It has 32 satellites (24 active at a time) that continuously broadcast signals with time stamp.
- Devices such as mobile, laptops, cars receive these signals and compare signals from 4 or more satellites.
- Trilateration: Based on this comparison, devices calculate distance between themselves and satellites to determine their location (longitude, latitude and altitude).
- GAGAN
- Space Based Augmentation System (SBAS) jointly developed by ISRO and AAI; GAGAN GEO footprint expands from Africa to Australia
- System of satellites and ground stations that provide GPS signal corrections;
- Only four Space-Based augmentation systems available in the world namely India (GAGAN), US (WAAS) Europe (EGNOS) and Japan (MSAS).
ISRO’s Third Launch Pad
- Union Cabinet approved the establishment of ‘Third Launch Pad’ (TLP) project at Satish Dhawan Space Centre of ISRO at Sriharikota, Andhra Pradesh.
- It is designed to support the launch of Next Generation Launch Vehicles (NGLV) and Launch Vehicle Mark-3 (LVM3) with a semi-cryogenic stage and upgraded NGLV configurations.
- It is also supported as a standby launch pad for the Second Launch Pad at Sriharikota.
- It is expected to be operational within 4 years.
- Significance:
- Increases Launch Capacity: Enhances launch frequency and supports future human spaceflight and space exploration missions.
- Advances India’s Space Vision: Essential for India’s long-term goals, including the Bharatiya Antariksh Station (BAS) by 2035 and an Indian Crewed Lunar Landing by 2040.
- Future Space Transportation: Ensures India meets evolving space transportation needs for the next 25-30 years.
Reasons for Choosing Sriharikota for Satellite Launch Pads
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Scramjet Engine
- A Scramjet engine (Supersonic Combustion Ramjet) is an improved version of the Ramjet, designed to operate at extremely high speeds.
- A ramjet is an air-breathing jet engine that relies on the vehicle’s forward motion to compress incoming air for combustion, eliminating the need for a rotating compressor
- It works by using supersonic airflow to generate thrust and functions at hypersonic speeds (Mach 5+)
- Key features:
- Air-Breathing Engine: Unlike traditional rocket engines, Scramjets use atmospheric oxygen for combustion, eliminating the need to carry heavy oxygen tanks.
- No Moving Parts: Scramjets rely on supersonic airflow, making them highly efficient for sustained high-speed travel.
- Significance:
- Next-generation hypersonic missiles with unmatched speed and accuracy.
- Faster air travel, potentially reducing flight times drastically.
- Low-cost satellite launches, making space access more affordable.
Mission in news
Chandrayaan 3
- India’s third lunar exploration mission, led by the Indian Space Research Organisation (ISRO).
- Objective: To demonstrate end-to-end capability in landing and roving on the lunar surface, specifically targeting the south pole.
- Launch Vehicle:
- GSLV Mk III (Geosynchronous Satellite Launch Vehicle Mark III).
- Height: 43.43 meters.
- Payload capacity: Up to 4,000 kg to Geosynchronous Transfer Orbit (GTO).
- Components:
- Lander: Equipped with navigation, hazard detection, and landing technology.
- Rover: Designed to explore the lunar surface and conduct scientific experiments.
- Propulsion Module: Provides necessary thrust for the journey from Earth to lunar orbit.
- Modules and Corresponding Payloads
- Lander (Vikram):
- Payloads:
- Chandra’s Surface Thermophysical Experiment (ChaSTE): Measures thermal conductivity and temperature.
- Instrument for Lunar Seismic Activity (ILSA): Detects seismic activities on the Moon.
- Langmuir Probe (LP): Measures the plasma density near the lunar surface.
- Payloads:
- Rover (Pragyan):
- Payloads:
- Alpha Particle X-ray Spectrometer (APXS): Analyzes the elemental composition of the lunar surface.
- Laser Induced Breakdown Spectroscope (LIBS): Identifies elements present on the lunar surface.
- Propulsion Module:
- Payload:
- Spectro-polarimetry of Habitable Planet Earth (SHAPE): Studies the spectral and polarimetric characteristics of Earth from lunar orbit.
NISAR (NASA-ISRO-SAR)
- A collaborative mission between the National Aeronautics and Space Administration (NASA) and the Indian Space Research Organisation (ISRO) scheduled for launch in 2024.
- Objective: To utilize advanced radar technology for comprehensive monitoring of Earth’s dynamic surfaces and ecosystems.
- Technical Specifications:
- Dual-frequency Radar System:
- L-band (longer wavelength) (ISRO Contribution): Offers superior ground penetration, ideal for biomass assessment and subsurface structure analysis.
- S-band (shorter wavelength) (NASA Contribution): Provides high-resolution imagery for detailed observations.
- High-Resolution Data: Generates topographic data with resolutions ranging from 3 to 10 meters, enabling precise mapping.
- Temporal Resolution: Repeats observations every 6 days, facilitating the monitoring of changes over time.
Artemis Accords
- The Artemis Accords are a set of international agreements outlining principles for peaceful cooperation in exploring the Moon, Mars, and other celestial bodies.
- Established by the US (NASA) with several other countries.
- India is a member! It became the 27th nation to sign on.
- Key points:
- Promotes peaceful exploration and scientific discovery.
- Encourages transparency and public awareness.
- Establishes guidelines for resource utilization in space.
- Not a binding treaty, but promotes collaboration.
Mission SCOT
- It is the world’s first commercial satellite for surveillance of Resident Space Objects (as small as 5cm) orbiting the Earth to ensure safer space operations. .
- It aims to improve space safety, optimise traffic management and strengthen national security initiatives.
- The SCOT satellite has been launched onboard SpaceX Transporter-12 mission.
- SCOT will be deployed in a sun-synchronous orbit. This will enable it to track objects in Low Earth Orbit (LEO) with greater efficiency as compared to the existing sensors.
PUNCH Mission
- NASA is gearing up for a new and first-of-its-kind solar mission called PUNCH mission that will closely observe the solar atmosphere
- The Polarimetry to Unify the Corona and Heliosphere (PUNCH) mission will be launched by SpaceX.
- Time Period: The expected mission life is two years.
- It is the first time that a solar mission has been specifically designed to make use of the polarisation of light to measure the corona and solar wind, that too, in 3D.
- It will provide scientists with new information which could lead to more accurate predictions about the arrival of space weather events on Earth and impact on humanity’s robotic explorers in space.
- It will measure polarised light using polarising filters, enabling scientists to look into the inner solar system.
GAIA Mission
- The European Space Agency (ESA) has officially decommissioned its Global Astrometric Interferometer for Astrophysics (GAIA) mission.
- It aimed to create the largest and most precise 3D map of the Milky Way by surveying about 1% of its 100 billion stars.
- It was launched in 2013.
- Position: Gaia orbits the Sun at Lagrange Point 2, about 1.5 million kilometers (930,000 miles) from Earth.
Moonlight Programme
- The European Space Agency has launched the Moonlight Lunar Communications and Navigation Services (LCNS) programme.
- Objective: To support over 400 moon missions planned by space agencies and private companies over the next 20 years.
- Structure: A constellation of five satellites orbiting the Moon.
- Benefits:
▪ Enable precise and autonomous lunar landings and surface mobility.
▪ Facilitate high-speed communication and data transfer between Earth and the Moon.
▪ Provide coverage at the Moon’s South Pole. - Timeline: Initial services to begin by the end of 2028, with full operational capacity by 2030.
Analog Space Mission
- ISRO has launched India’s first analog space mission in Leh, Ladakh, to prepare for lunar mission experiments.
- It was developed in collaboration with ISRO’s Human Spaceflight Center, AAKA Space Studio, the University of Ladakh, and IIT Bombay.
About Analog Missions
- Analog space missions simulate the physical and operational conditions of space environments on Earth.
- Purpose:
▪ Testing new technologies, equipment, and vehicles.
▪ Training astronauts for future missions.
▪ Studying the behavioral and psychological effects of isolation and confinement.
▪ Conducting experiments in space-like conditions. - Why Leh (Ladakh)? Its dry, cold climate, barren land, high altitude, and isolation resemble Martian and lunar landscapes.
RISE Mission
- RISE, the European Space Agency’s first in-orbit servicing mission, represents a major step toward enabling refueling, refurbishment, and in-orbit assembly— key elements for building a circular economy in space.
- Launch Year: 2028
- Capabilities: Docking with geostationary satellites and controlling their orbits.
- Mission Scope: RISE will ascend to the geostationary graveyard orbit, about 100 km above the active satellite zone, where decommissioned satellites are parked.
Note: The circular space economy mirrors the principles of a circular economy, focusing on reducing waste and improving resource efficiency in space.
ADITYA-L1 MISSION
- ISRO’s Aditya-L1 completes its first halo orbit around the Sun-Earth L1 point
Key Highlights:
- Aditya-L1 was placed into its halo orbit in early 2024
- It took 178 days to complete one revolution around the Lagrange L1 point
- Lagrange Points:
- Positions where the gravitational pull of two large masses equals the centripetal force required for a small object to move with them
- There are five Lagrange points in a two-body system: L1, L2, L3, L4, and L5
- L4 and L5 are considered stable
About Halo Orbit
- A halo orbit is a repeating, three-dimensional orbit around one of the L1, L2, or L3 Lagrange points in a three-body system
Advantages of placing Aditya-L1 in a Halo Orbit:
- Ensures a mission lifetime of 5 years
- Minimizes fuel usage by reducing station-keeping maneuvers
- Maintains a clear, uninterrupted view of the Sun
About Aditya-L1 Mission (Launched in 2023)
- India’s first space mission dedicated to studying the Sun
- Objectives:
- Investigate the Sun’s corona, solar emissions, solar winds, flares, and Coronal Mass Ejections (CMEs)
- Enable continuous imaging of the Sun
- Payloads:
- Equipped with 7 payloads, including:
- Visible Emission Line Coronagraph (VELC)
- Solar Ultraviolet Imaging Telescope (SUIT)
- And others
- Equipped with 7 payloads, including:
Dragonfly Mission
- It is the fourth mission in NASA’s New Frontiers Program, alongside New Horizons, Juno, and OSIRIS-REx
- Objective: It is an astrobiology mission to Titan aimed at evaluating its potential for microbial life and examining its prebiotic chemistry at multiple sites
- It marks the first time NASA will fly a vehicle for science on another planetary body
- It will reach Titan in 2034
Technical Specifications
- Design: Dragonfly is a “dual quadcopter” about the size of a car, capable of traveling tens of kilometers on Titan in under an hour
- Power Source: Dragonfly will use a radioisotope power system, like the one used by the Curiosity rover on Mars
About Titan
- It is Saturn’s largest moon, featuring an Earth-like cycle of liquid flowing across its surface and being the only moon with a dense atmosphere
ISRO’S RLV LEX-02 Mission
About Reusable Landing Vehicle (RLV) LEX-02 developed by ISRO
- It is the second in a series of test flights designed to showcase the autonomous landing capability of a reusable launch vehicle (RLV)
- The mission featured a winged vehicle named Pushpak, which was lifted to an altitude of 4.5 kilometers by an Indian Air Force Chinook helicopter
- Pushpak was released and had to autonomously execute a series of maneuvers to land accurately on the runway
About Reusable Landing Vehicle
- The reusable launch vehicle is essentially a spaceplane with a low lift-to-drag ratio, which means it must approach at steep glide angles and land at high speeds of 350 km/h
Lunar Polar Exploration Mission (LUPEX) Mission
- It is a joint mission of Japan Aerospace Exploration Agency (JAXA) and Indian Space Research Organisation (ISRO)
- Objective: To explore the Moon’s southern polar region for water and other elements, possibly in the form of surface ice
- Contributions: For the LUPEX mission, the launch vehicle and rover are supposed to be contributed by the Japanese agency, while the lander will come from ISRO
- It will also carry instruments from NASA and the European Space Agency (ESA)
Defence
Weapons/Systems in News (India)
Pinaka Multiple Rocket Launch Systems (MRLS)
- It is a battle-proven, all-weather, indirect area fire Artillery Weapon System.
- Developed by DRDO’s Armament Research and Development Establishment (ARDE).
- First used during the Kargil War, where it successfully neutralized Pakistan Army positions on the mountain tops.
- It delivers a variety of warheads, including high-explosive and submunitions.
- It has a range of 60 to 75 kilometers.
Nag Mark-2
- It is an indigenously developed anti-tank guided missile (ATGM) that works in all weather conditions.
- It is a fire-and-forget missile with lock-on after launch capability.
- Developed by: Defence Research and Development Organisation (DRDO).
- The missile is launched from NAMICA (Nag Missile Carrier), an anti-tank armored vehicle used by the Indian Army.
- Estimated range: 7 to 10 kilometers.
Vertically Launched Short-Range Surface-to-Air Missile (VL-SRSAM)
- Developed by: Defence Research and Development Organisation (DRDO).
- This quick-reaction missile is capable of neutralizing various aerial threats at close ranges, including sea-skimming targets.
- Initially designed for the Indian Navy with a strike range of 40 km, it has now been enhanced to attack targets up to 80 km.
- Additionally, it is being developed for the Indian Air Force to safeguard its air bases.
- It is capable of reaching Mach 4.5 and can achieve a maximum altitude of 16 km.
Bhargavastra
- India’s first indigenous micro-missile system, developed by Economic Explosives Ltd., is specifically designed to counter the threat posed by swarm drones.
- This system can be rapidly deployed on mobile platforms and effectively target threats over 2.5 km.
- It has the capability to detect small flying objects from distances exceeding 6 km and neutralize them using guided micro munitions.
- The system is capable of launching more than 64 micro missiles simultaneously.
- It is built to operate across diverse terrains, including high-altitude regions, it meets the specialized needs of the armed forces.
SANJAY System
- Sanjay is an automated surveillance system that combines real-time data from ground and aerial sensors to create a unified view of the battlefield. This helps commanders make quick, informed decisions during both conventional and unconventional warfare.
- Developed by: Indian Army and Bharat Electronics Limited (BEL).
Advanced Ballistic for High Energy Defeat (ABHED) Jackets
- These jackets are made from polymers and indigenous boron carbide ceramic material.
- Developed by DRDO and IIT Delhi.
- They offer 360-degree protection with modular design and front/rear armour plates.
- Their weight ranges from 8.2 kg to 9.5 kg for different BIS levels.
India’s Fourth Nuclear Submarine
- India’s fourth nuclear-powered ballistic missile submarine (SSBN), referred to as S4, was launched into water at the Ship Building Centre in Visakhapatnam.
- S4 features about 75% indigenous content.
- It is armed exclusively with K-4 nuclear ballistic missiles (range: 3,500 km).
- India currently has two SSBNs operational: INS Arihant (commissioned in 2016) and INS Arighaat (commissioned in 2024).
- The third SSBN Aridhman is undergoing sea trials and is expected to be commissioned next year.
INS ARIGHAAT
- It is India’s second indigenously built nuclear-powered ballistic missile submarine (SSBN).
- It joins INS Arihant to strengthen India’s nuclear triad.
- It was constructed at the Indian Navy’s Ship Building Centre (SBC) in Visakhapatnam.
Features:
- It has a length of 111.6 meters and a submerged displacement of 6,000 tons.
- It has a seven-blade propeller powered by an 83-MW pressurised light water reactor using enriched uranium.
- It can carry up to 12 K-15 SLBMs, each with a range of 750 km.
RHUMI-1
- India’s first reusable hybrid rocket RHUMI-1 was launched from Thiruvidandhai in Chennai.
- RHUMI-1 was developed by Tamil Nadu-based startup Space Zone India in collaboration with the Martin Group.
- It was launched into a sub-orbital trajectory using a mobile launch system.
Key Features of RHUMI-1
- RHUMI-1 is a hybrid rocket engine that integrates both solid and liquid propellants.
- It is equipped with an electrically triggered parachute system, which is an advanced and eco-friendly descent mechanism.
- It has an adjustable launch angle (0 to 120 degrees), allowing for precise trajectory control.
- It is completely free of pyrotechnics (fireworks) and TNT (Trinitrotoluene), making it environmentally friendly.
Zorawar Tank
- It has been indigenously developed by the Defence Research and Development Organisation (DRDO) along with Larsen & Toubro (L&T).
- It is named after the great military general Zorawar Singh Kahluria.
- It is a lightweight tank with a maximum weight of 25 tonnes.
- It features advanced technologies such as artificial intelligence (AI) and drone integration.
- It is amphibious and can operate in varied terrain.
Rudram-1 Missile
- It is an air-to-surface missile developed by the Defence Research and Development Organisation (DRDO).
- The IAF’s Sukhoi-30MKI fighter jets serve as its launch platform.
- It can be launched from altitudes ranging from 500 meters to 15 kilometers, with a range of up to 250 kilometers.
- It is equipped with Inertial Navigation System (INS), GPS navigation, and a Passive Homing Head to precisely strike radiation-emitting targets.
Astra Mark 1 Missile
- It is a Beyond-Visual-Range (BVR) air-to-air missile.
- It will be deployed on fighter jets of the Indian Air Force and Indian Navy.
- It has been indigenously developed by DRDO and manufactured by Bharat Dynamics Limited (BDL).
- It has a range of 80 to 110 km in a head-on chase.
- It can travel at a speed of Mach 4.5.
GAURAV
- It is an air-launched, 1000-kg glide bomb capable of precisely hitting long-distance targets.
- It uses an Inertial Navigation-based guidance system.
- It can be integrated with fighter jets.
- It has been designed and developed indigenously by the Research Centre Imarat (RCI), Hyderabad.
Indigenous Technology Cruise Missile (ITCM) Flight Tested
- It has been developed by the Aeronautical Development Establishment of DRDO, with contributions from other laboratories and Indian industries.
- It is a long-range subsonic cruise missile designed to hit targets with precision.
- It is powered by an indigenous propulsion system.
✓ A subsonic cruise missile flies at a speed lower than that of sound (<1 Mach).
Agni Prime Successfully Flight-Tested
- It is a surface-to-surface ballistic missile.
- It is a nuclear-capable, two-stage canisterised missile with a maximum range of 1,000 to 2,000 km.
- It is lighter than all previous missiles in the Agni series.
Submersible Platform for Acoustic Characterisation and Evaluation (SPACE)
- It is a premier testing and evaluation hub for sonar systems for the Indian Navy.
- It has been set up by DRDO.
- It consists of two distinct platforms:
A) Floating Platform
B) Submersible Platform (submersible up to 100m depth) - It will bolster anti-submarine warfare research capabilities.
Project 28
- Objective: To build four indigenous Anti-Submarine Warfare (ASW) corvettes, also known as Kamorta-class corvettes.
- These four ASWs are: INS Kamorta, INS Kadmatt, INS Kiltan, and INS Kavaratti.
- These ships can be deployed in nuclear, biological, and chemical warfare conditions.
- Designed by: Indian Navy’s Directorate of Naval Design
- Built by: Garden Reach Shipbuilders & Engineers (GRSE), Kolkata
Nagastra-1
- It is India’s first indigenous loitering munition (suicide drone).
- It has been developed by Solar Industries, Nagpur.
- It has the capacity to carry a 1-kilogram warhead.
- It can carry out GPS-enabled precision strikes with an accuracy of up to 2 meters.
- It has an indigenous content of over 75%.
- It features a parachute recovery mechanism.
RudraM-II Missile
- It is an indigenously developed, solid-propelled, air-launched missile system.
- It has been designed for air-to-surface operations.
- It has been developed by the Defence Research and Development Organisation (DRDO).
Weapon Development in News – World
Dragon Drone
- Dragon drones are powerful UAVs equipped with thermite and rain down fire from the sky
- Thermite is a mixture of aluminium and iron oxide.
- When ignited, it produces a self-sustaining reaction that is extremely difficult to extinguish.
- Dragon Drones were used by Ukraine against Russia in the ongoing Russia-Ukraine War.
THAAD Missile Defence System
- It is an advanced defense system that can destroy short, medium, and intermediate-range ballistic missiles.
- Developed by Lockheed Martin Corporation.
- Employs a ‘hit-to-kill’ approach to target missiles.
- Its target range varies between 150–200 kilometers.
Crystal Maze 2 (also known as ROCKS)
- It is a medium-range ballistic missile.
- It has been developed by Israel.
- It is an air-to-surface missile with a strike range of over 250 km.
- It has the capability to strike high-value stationary and relocatable targets in GPS-denied environments.
C-Dome Defense System
- It has been developed by Israel.
- It is a naval version of Israel’s Iron Dome air defense system.
- It is designed to shield against missile and rocket attacks.
- Unlike the Iron Dome which features its own radar, C-Dome is integrated into ship’s radar to detect incoming targets.
Hermes-900
- It is an advanced, Medium Altitude Long Endurance (MALE) unmanned aerial vehicle.
- It is of Israeli origin.
- It is also known as Drishti-10 drone.
- It features Automatic Take Off and Landing (ATOL) capability, Terrain Avoidance Warning System (TAWS), Synthetic Aperture Radar (SAR).
- It can be employed for Intelligence, Surveillance, Target Acquisition and Reconnaissance (ISTAR) missions.
Igla-S Air Defense System
- It is a man-portable air defense system (MANPADS).
- It has been developed by Russia.
- It is a handheld, very short range defense system (VSHORAD).
It has an interception range of up to 6 kms and can destroy targets at altitudes of up to 3.5 km.
MQ-9B Drones
- These drones are Unmanned Aerial Vehicles (UAVs) with high altitude and long endurance capabilities, created for surveillance, reconnaissance, and precision strike operations.
- They have a maximum endurance of 40 hours and can hit targets on land, sea, and air.
- They have two variants: SkyGuardian and SeaGuardian.
Exercises in News
- Dharma Guardian – Joint military exercise between India and Japan.
- Ekuverin – Bilateral military exercise between India and the Maldives.
- Cyclone 2025 – Joint military exercise between India and Egypt.
- La Perouse – Multilateral naval exercise hosted by France, involving India, Australia, Canada, USA, Indonesia, Malaysia, UK, and Singapore.
- KAZIND 2024 – Joint military exercise between India and Kazakhstan.
- Naseem Al Bahr – Bilateral naval exercise between India and Oman.
- Garud Shakti – Joint special forces exercise between India and Indonesia.
- VINBAX 2024 – Bilateral army exercise between India and Vietnam.
- SIMBEX-2024 – Bilateral maritime exercise between India and Singapore.
- Poorvi Prahar – High-intensity tri-services exercise conducted by the Indian Army.
- Sanyukt Vimochan 2024 – Humanitarian Assistance and Disaster Relief (HADR) exercise conducted by the Indian Army.
- SAREX-24 – National maritime search and rescue exercise conducted by the Indian Coast Guard (ICG).
- Exercise Antariksha Abhyas 2024 – India’s first-ever space exercise conducted by the Defence Space Agency under the Ministry of Defence.
- Rim of the Pacific (RIMPAC)- World’s largest biennial maritime exercise, held in Hawaii.Led by the US Navy; 29 countries participated, including India.
- Exercise Pitch Black- Biennial multinational air exercise hosted by the Royal Australian Air Force.
- Exercise Mitra Shakti- Annual joint exercise between India and Sri Lanka.
- Exercise Tarang Shakti- India’s first multinational air exercise, inspired by the US Red Flag.
- Exercise Udara Shakti- Bilateral air exercise between India and Malaysia.
- Exercise Eastern Bridge- Bilateral air exercise between IAF and Oman’s RAFO.
- Exercise Al Najah- Biennial joint military exercise between India and Oman since 2015.
- Tarkash Exercise- India–US joint counter-terrorism exercise.
- Shakti Exercise- Biennial India–France military exercise
- HOPEX Exercise- Type: India–Egypt Air Force joint exercise
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