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Science and Technology (SSC, Railway, Police & All State exam)Chapter Unit

Launch Vehicles

Introduction to Launch Vehicles

  1. Definition:

    • A launch vehicle is a rocket-powered system designed to transport payloads (e.g., satellites, crew, scientific instruments) into space.
  2. Components of a Launch Vehicle:

    • Payload: The cargo being carried (e.g., satellites, instruments).
    • Propulsion System:
      • Provides the thrust to escape Earth’s gravity.
      • Types: Solid, liquid, cryogenic, and hybrid propellants.
    • Stages:
      • Multistage structure for sequential thrust generation.
      • Common types: Two-stage, three-stage, and modular systems.
    • Control Systems:
      • Ensures stability, navigation, and trajectory control.

Types of Launch Vehicles

  1. Based on Reusability:

    • Expendable Launch Vehicles (ELVs):
      • Single-use rockets.
      • Examples: PSLV, GSLV.
    • Reusable Launch Vehicles (RLVs):
      • Designed for multiple uses to reduce costs.
      • Examples: SpaceX’s Falcon 9, ISRO’s RLV-TD.
  2. Based on Payload Capacity:

    • Small-lift Vehicles:
      • Carry payloads up to 2,000 kg.
      • Example: SSLV (India).
    • Medium-lift Vehicles:
      • Carry payloads between 2,000–20,000 kg.
      • Example: PSLV.
    • Heavy-lift Vehicles:
      • Carry payloads over 20,000 kg.
      • Example: GSLV Mk III.
  3. Based on Orbit Type:

    • Low Earth Orbit (LEO): Altitude 180–2,000 km.
    • Geostationary Transfer Orbit (GTO): Used for GEO satellites.
    • Polar Orbit: Over Earth’s poles for global coverage.

History of Indian Launch Vehicles

  1. Early Years:

    • 1963: India launched its first sounding rocket, Nike-Apache, from the Thumba Equatorial Rocket Launching Station (TERLS).
    • 1980: First indigenous launch vehicle, SLV-3, successfully placed the Rohini Satellite RS-1 in orbit.
  2. Major Milestones:

    • Satellite Launch Vehicle (SLV):
      • Used for experimental launches.
      • Payload capacity: 40 kg to LEO.
    • Augmented Satellite Launch Vehicle (ASLV):
      • Improved payload capacity (150 kg to LEO).
      • Key mission: ASLV-D3 (1992).

PSLV (Polar Satellite Launch Vehicle)

  1. Introduction:

    • Developed by ISRO in the 1990s.
    • Known as the "Workhorse of ISRO."
    • Used for launching satellites into Sun-synchronous and polar orbits.
  2. Technical Features:

    • Four Stages:
      • 1st stage: Solid propellant.
      • 2nd stage: Liquid propellant.
      • 3rd stage: Solid propellant.
      • 4th stage: Liquid propellant.
    • High accuracy for multi-payload launches.
  3. Notable Missions:

    • PSLV-C37 (2017):
      • Launched 104 satellites in a single mission (world record).
    • Chandrayaan-1 (2008):
      • India’s first lunar mission.
  4. Variants:

    • PSLV-G (Standard configuration).
    • PSLV-XL (Extended configuration for heavier payloads).

GSLV (Geosynchronous Satellite Launch Vehicle)

  1. Introduction:

    • Developed for launching heavier payloads into geostationary transfer orbits.
    • Incorporates cryogenic technology for enhanced performance.
  2. Technical Features:

    • Three Stages:
      • 1st stage: Solid propellant.
      • 2nd stage: Liquid propellant.
      • 3rd stage: Cryogenic upper stage (CUS).
    • Payload capacity: ~2,500 kg to GTO.
  3. Significant Missions:

    • GSLV-F08 (2018):
      • Launched GSAT-6A communication satellite.
    • GSLV-D5 (2014):
      • First successful cryogenic stage mission.

Table: Comparison of PSLV and GSLV

FeaturePSLVGSLV
Orbit TypePolar/Sun-synchronousGeostationary
Payload CapacityUp to 1,750 kg to SSOUp to 2,500 kg to GTO
Notable MissionPSLV-C37 (104 satellites)Chandrayaan-2
StagesFourThree

GSLV Mk III (LVM3)

  1. Introduction:

    • Known as "Bahubali", India’s heavy-lift launch vehicle.
    • Designed to carry heavier payloads and support ambitious missions such as crewed spaceflights.
    • Payload capacity:
      • ~4,000 kg to Geostationary Transfer Orbit (GTO).
      • ~10,000 kg to Low Earth Orbit (LEO).
  2. Technical Features:

    • Three Stages:
      • 1st stage: Two solid rocket boosters (S200).
      • 2nd stage: Liquid core stage (L110).
      • 3rd stage: Cryogenic upper stage (C25).
    • Advanced avionics for precise navigation and control.
  3. Notable Missions:

    • Chandrayaan-2 (2019):
      • Carried a lander, rover, and orbiter to the Moon.
    • Gaganyaan Program (Upcoming):
      • Will launch India's first crewed spaceflight mission.
    • Launch of OneWeb satellites (2022):
      • Deployed 36 satellites for a global communication network.

Small Satellite Launch Vehicle (SSLV)

  1. Introduction:

    • Developed for launching small satellites cost-effectively and on-demand.
    • Payload capacity: 500 kg to Low Earth Orbit (LEO).
  2. Features:

    • Compact size for quick assembly and integration.
    • Capable of launching from small launch sites.
    • Uses solid propellant for all stages.
  3. Notable Missions:

    • SSLV-D2 (2023):
      • Successfully placed satellites into orbit after addressing issues from the maiden flight.

Reusable Launch Vehicles (RLV)

  1. Introduction:

    • Designed to reduce the cost of access to space by reusing launch systems.
    • ISRO’s RLV is being developed as a winged body prototype.
  2. Key Tests:

    • RLV-TD HEX-01 (2016):
      • Demonstrated atmospheric re-entry and autonomous landing capabilities.
  3. Future Plans:

    • Development of a fully operational reusable launch vehicle for satellite deployment.

Evolution of Propulsion Systems in India

  1. Solid Propulsion:

    • Used in early rockets like SLV and the first stages of PSLV and GSLV.
    • Simple design and reliable performance.
  2. Liquid Propulsion:

    • Developed for higher efficiency and control during flight.
    • Used in the second stages of PSLV and GSLV.
  3. Cryogenic Propulsion:

    • Advanced technology using super-cooled fuels (e.g., liquid hydrogen and liquid oxygen).
    • Essential for heavy-lift vehicles like GSLV and GSLV Mk III.
    • First indigenous cryogenic engine: CE-7.5, used in GSLV-D5 (2014).
  4. Semi-Cryogenic Propulsion (Under Development):

    • Combines liquid oxygen with refined kerosene for improved performance.
    • Will be used in future heavy-lift launch vehicles.

International Collaboration and Commercial Launches

  1. International Partnerships:

    • ISRO has collaborated with global space agencies like NASA, CNES (France), and Roscosmos (Russia).
    • Joint missions include:
      • NISAR (NASA-ISRO Synthetic Aperture Radar): Scheduled for 2024.
      • Chandrayaan-1: Carried payloads from international agencies.
  2. Commercial Launch Services:

    • ISRO’s commercial arm, Antrix Corporation, and NewSpace India Limited (NSIL):
      • Offer cost-effective satellite launches for international clients.
    • India has launched satellites for over 30 countries using PSLV and GSLV.

Challenges and Future of Indian Launch Vehicles

  1. Challenges:

    • Development of reusable systems to compete with global players like SpaceX.
    • Advancing payload capacity to cater to interplanetary missions and commercial demands.
  2. Future Goals:

    • Launching heavier payloads with next-generation vehicles.
    • Enhancing reusability and developing environmentally sustainable propulsion systems.
    • Supporting India’s human spaceflight and deep-space exploration programs.

Table: Comparison of Indian Launch Vehicles

Launch VehiclePayload CapacityNotable MissionsPurpose
PSLV1,750 kg to SSOChandrayaan-1, MOMEarth observation, science
GSLV2,500 kg to GTOGSAT series, Chandrayaan-2Communication, lunar missions
GSLV Mk III (LVM3)4,000 kg to GTO, 10,000 kg to LEOChandrayaan-2, OneWebHeavy payloads, crewed missions
SSLV500 kg to LEOSSLV-D2Small satellite launches
RLV (Prototype)ReusableRLV-TD HEX-01Cost reduction, reusability

Global Comparison of Launch Vehicles

  1. Key Global Launch Vehicles:

    • SpaceX Falcon 9 (USA):
      • First partially reusable launch vehicle.
      • Payload capacity:
        • 22,800 kg to Low Earth Orbit (LEO).
        • 8,300 kg to Geostationary Transfer Orbit (GTO).
    • Ariane 5 (Europe):
      • Developed by the European Space Agency (ESA).
      • Payload capacity:
        • 10,000 kg to GTO.
        • Notable for launching interplanetary missions and communication satellites.
    • Long March Series (China):
      • Family of rockets with varying capacities.
      • Example: Long March 5 can carry 25,000 kg to LEO.
    • Soyuz (Russia):
      • Known for reliability in manned and unmanned missions.
      • Used for International Space Station (ISS) resupply missions.
  2. India’s Competitive Edge:

    • Cost-effective solutions with high success rates.
    • Proven track record in launching satellites for international clients.

Key Achievements of Indian Launch Vehicles

  1. Mars Orbiter Mission (MOM):

    • Launched by PSLV-C25 in 2013.
    • India became the first nation to reach Mars on its maiden attempt.
    • Cost: $74 million (one of the cheapest Mars missions).
  2. PSLV-C37 (2017):

    • Set a world record by launching 104 satellites in a single mission.
  3. Chandrayaan Missions:

    • Chandrayaan-1 (2008):
      • Launched by PSLV; discovered water molecules on the Moon.
    • Chandrayaan-2 (2019):
      • Launched by GSLV Mk III; included an orbiter, lander, and rover.
  4. Commercial Launches:

    • Over 300 foreign satellites launched using PSLV and GSLV.
  5. Cryogenic Technology Development:

    • Indigenous cryogenic engines used in GSLV-D5 (2014) marked a major technological milestone.

Future Indian Launch Vehicles

  1. Next-Generation Launch Vehicle (NGLV):

    • Designed for heavy payloads and reusability.
    • Payload capacity: Up to 10,000 kg to GTO.
    • Applications: Interplanetary missions, crewed spaceflights, and large-scale commercial launches.
  2. Semi-Cryogenic Engines:

    • SCE-200 engine under development.
    • Features:
      • Uses refined kerosene and liquid oxygen.
      • Offers higher efficiency and thrust.
  3. Hypersonic Reusable Vehicles:

    • Focus on reducing the cost of access to space.
    • Integration of scramjet technology for higher speeds.

Environmental Considerations in Launch Vehicles

  1. Challenges:

    • Rocket launches produce emissions contributing to air pollution.
    • Space debris from expended rocket stages and defunct satellites.
  2. Solutions:

    • Development of reusable rockets (e.g., SpaceX’s Falcon 9, ISRO’s RLV-TD).
    • Use of cleaner fuels like hydrogen and bio-propellants.
    • Designing satellites and rockets for controlled deorbiting.

Indian Launch Vehicles

  • India has made remarkable strides in developing cost-effective and reliable launch vehicles.
  • The diversity in launch systems, from PSLV for small satellites to GSLV Mk III for heavy payloads, enables ISRO to cater to a wide range of missions.
  • Future advancements in semi-cryogenic and reusable technologies will further strengthen India’s position in the global space industry.

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