CHANDRAYAAN 3
A Mission Of Hope For The Future Of Space
Exploration.
Chandrayaan 3 is India's third lunar
mission to soft land on the lunar south
pole region. The mission will conduct
scientific experiments to study the lunar
geology, atmosphere, and environment.
Introduction Of
Chandrayaan 3
Three Mission
Objectives
Demonstrate safe and
soft landing on the
lunar surface
Conduct rover
operations on the
Moon
Conduct on-site
experiments on the
lunar surface
1 2 3
Key Technologies
Hazard Detection and Avoidance
Lander Hazard Detection & Avoidance
Camera and Processing Algorithm
Landing Leg Mechanism.
Inertial Measurement
Laser Gyro based Inertial referencing and
Accelerometer package
Altimeters
Laser & RF based Altimeters
Propulsion System
800N Throttleable Liquid Engines, 58N
attitude thrusters & Throttleable Engine
Control Electronics
Velocimeters
Laser Doppler Velocimeter & Lander
Horizontal Velocity Camera
Navigation, Guidance & Control
Powered Descent Trajectory design and
associate software elements
1 2 3
4 5 6
Lander Special Tests
Integrated Cold Test: For the demonstration of
Integrated Sensors & Navigation performance
test using helicopter as test platform
1
Integrated Hot test: For the demonstration of
closed loop performance test with sensors,
actuators and NGC using Tower crane as test
platform
2
Lander Leg mechanism performance test on a
lunar simulant test bed simulating different touch
down conditions.
3
Mission Components
Propulsion module
This module is responsible for carrying the
lander and rover configuration to the
Moon. It also has a scientific payload that
will study the Earth from lunar orbit.
Lander module
This module will land on the Moon and
deploy the rover. It also has a scientific
payload that will study the lunar surface.
Rover
This is a small, mobile vehicle that will
conduct on-site experiments on the lunar
surface. It is equipped with a variety of
scientific instruments, including a
seismometer, a spectrometer, and a
camera.
Specifications For Chandrayaan-3
Sl No. Parameter Specifications Sl No. Parameter Specifications
1. Mission Life (Lander & Rover) One lunar day (~14 Earth days) 7. Communication
1.Propulsion Module: Communicates with IDSN
2.Lander Module: Communicates with IDSN and Rover. Chandrayaan-2 Orbiter is also planned for
contingency link.
3.Rover: Communicates only with Lander.
2. Landing Site (Prime) 4 km x 2.4 km 69.367621 S, 32.348126 E 8. Lander Sensors
1.Laser Inertial Referencing and Accelerometer Package (LIRAP)
2.Ka-Band Altimeter (KaRA)
3.Lander Position Detection Camera (LPDC)
4.LHDAC (Lander Hazard Detection & Avoidance Camera)
5.Laser Altimeter (LASA)
6.Laser Doppler Velocimeter (LDV)
7.Lander Horizontal Velocity Camera (LHVC)
8.Micro Star sensor
9.Inclinometer & Touchdown sensors
3. Science Payloads
1.Lander:Radio Anatomy of Moon Bound Hypersensitive ionosphere and
Atmosphere (RAMBHA)
2.Chandra’s Surface Thermo physical Experiment (ChaSTE)
3.Instrument for Lunar Seismic Activity (ILSA)
4.Laser Retroreflector Array (LRA) Rover:
5.Alpha Particle X-Ray Spectrometer (APXS)
6.Laser Induced Breakdown Spectroscope (LIBS) Propulsion Module:
7.Spectro-polarimetry of HAbitable Planet Earth (SHAPE)
9. Lander Actuators Reaction wheels – 4 nos (10 Nms & 0.1 Nm)
4. Two Module Configuration
1.Propulsion Module (Carries Lander from launch injection to Lunar orbit)
2.Lander Module (Rover is accommodated inside the Lander)
10. Lander Propulsion System
Bi-Propellant Propulsion System (MMH + MON3), 4 nos. of 800 N Throttleable engines & 8 nos. of
58 N; Throttleable Engine Control Electronics
5. Mass
1.Propulsion Module: 2148 kg
2.Lander Module: 1752 kg including Rover of 26 kg
3.Total: 3900 kg
11. Lander Mechanisms
1.Lander leg
2.Rover Ramp (Primary & Secondary)
3.Rover
4.ILSA, Rambha & Chaste Payloads
5.Umbilical connector Protection Mechanism,
6.X- Band Antenna
6. Power generation
1.Propulsion Module: 758 W
2.Lander Module: 738W, WS with Bias
3.Rover: 50W
12. Lander Touchdown specifications
1.Vertical velocity: 2 m / sec
≤
2.Horizontal velocity: 0.5 m / sec
≤
3.Slope: 120
≤
Objectives Of Scientific Payloads
SI. No Lander Payloads Objectives
1.
Radio Anatomy of Moon Bound
Hypersensitive ionosphere and
Atmosphere (RAMBHA)
Langmuir probe (LP)
To measure the near surface plasma (ions and
electrons) density and its changes with time
2.
Chandra’s Surface Thermo physical
Experiment (ChaSTE)
To carry out the measurements of thermal properties of lunar surface near
polar region.
3.
Instrument for Lunar Seismic Activity
(ILSA)
To measure seismicity around the landing site and delineating the structure of
the lunar crust and mantle.
4. LASER Retroreflector Array (LRA) It is a passive experiment to understand the dynamics of Moon system.
SI. No Rover Payloads Objectives
1.
LASER Induced Breakdown
Spectroscope (LIBS)
Qualitative and quantitative
elemental analysis & To derive
the chemical Composition and
infer mineralogical
composition to further our
understanding of Lunar-
surface.
2.
Alpha Particle X-ray
Spectrometer (APXS)
To determine the elemental
composition (Mg, Al, Si, K,
Ca,Ti, Fe) of Lunar soil and
rocks around the lunar landing
site.
Sl. No
Propulsion Module
Payload
Objectives
1.
Spectro-polarimetry of HAbitable
Planet Earth (SHAPE)
Future discoveries of
smaller planets in
reflected light would
allow us to probe into
variety of Exo-planets
which would qualify for
habitability (or for
presence of life).
Launch And
Landing Of
Chandrayaan-3
Chandrayaan-3 was launched on July 14,
2023. It entered a lunar transfer orbit on
July 15, 2023. The lander is expected to
land on the lunar south pole region on
August 23 or August 24, 2023.
Event Date
Launch July 14, 2023
Lunar transfer
orbit
July 15, 2023
Landing on the
lunar south pole
region
August 23-24,
2023
First Indian mission
to land on the lunar
south pole region
First Indian mission
to carry a rover Advances India's
space exploration
capabilities
Promotes
international
cooperation in
space exploration
The Significance
Of Chandrayaan-
3
Mission Life
Propulsion Module
3 to 6 months
1
Lander Rover
1 Lunar Day
1
Landing Site
69.36 degree S, 32.34 degree E; slightly off the
site for Chandrayaan-2
1
Integrated Module Phase
Lunar Transfer Trajectory
Injectio
n Orbit
EBNs
Lunar Orbit Insertion
Lunar Orbit
Lander
Deboost
Lander Propulsion
Model Separation
Touchdown
Mission Profile
Mission Profile
Animation of Chandrayaan-3
Chandrayaan-3 Earth Moon
The Earth-Moon average distance is
roughly 384,400 kilometers. To save
fuel, Chandrayaan-3 has chosen a
longer route to the Moon. This adjusted
path aims to ensure a gentle landing of
the mission's Vikram lander on the
Moon's South Pole area. The expected
timeline for this soft touchdown is
approximately 42 days after launch,
specifically around August 23 or 24.
Trajectory
01
02
03
04
05
06 07
Nominal Flight
Sequence
S.No Event Flight Time (s) Altitude (km)
Inertial Velocity
(km/s)
1 2xS200 Ignition 0.00 0.024 0.452
2 L110 Ignition 108.10 44.668 1.788
3 2xS200 Separation 127.00 62.171 1.969
4 PLF Separation 194.96 114.805 2.560
5 L110 Separation 305.56 175.352 4.623
6 C25 Ignition 307.96 176.573 4.621
7 C25 Shut-off 954.42 174.695 10.242
8 Satellite Separation 969.42 179.192 10.269
LVM3-M4-Chandrayaan-3 Mission Timeline
July 14, 2023
LVM3 M4 vehicle successfully launched Chandrayaan-3 into orbit. Chandrayaan-3,
in its precise orbit, has begun its journey to the Moon. Health of the Spacecraft is
normal.
July 22, 2023
The fourth orbit-raising maneuver (Earth-bound perigee firing) is completed. The
spacecraft is now in a 71351 km x 233 km orbit.
August 06, 2023
LBN#2 is successfully completed. The spacecarft is in 170 km x 4313 km orbit
around the moon
July 25, 2023
Orbit-raising maneuver performed on July 25, 2023. Next firing (TransLunar
Injection), is planned for August 1, 2023.
July 15, 2023
The first orbit-raising maneuver (Earthbound firing-1) is successfully
performed at ISTRAC/ISRO, Bengaluru. Spacecraft is now in 41762 km x
173 km orbit.
July 17, 2023
The second orbit-raising maneuver performed. The spacecraft is now in
41603 km x 226 km orbit.
August 05, 2023
Chandrayaan-3 is successfully inserted into the lunar orbit. The orbit
achieved is 164 km x 18074 km, as intended.
August 01, 2023
The spacecraft is inserted into the translunar orbit. The orbit achieved is
288 km x 369328 km. Lunar-Orbit Insertion (LOI) is planned for Aug 5,
2023.
Chandrayaan-3 Capture First Image
The Moon, as viewed by Chandrayaan-3 during Lunar Orbit Insertion
Conclusion Of
Chandrayaan
3
Chandrayaan 3 was a successful mission that
achieved its objectives of soft landing on the
lunar south pole region and conducting
scientific experiments. The mission has
furthered India's space exploration capabilities
and has helped to gain a better understanding
of the Moon.
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Copy of SlideEgg_200407-Chandrayaan 3.pptx

  • 1. CHANDRAYAAN 3 A Mission Of Hope For The Future Of Space Exploration.
  • 2. Chandrayaan 3 is India's third lunar mission to soft land on the lunar south pole region. The mission will conduct scientific experiments to study the lunar geology, atmosphere, and environment. Introduction Of Chandrayaan 3
  • 3. Three Mission Objectives Demonstrate safe and soft landing on the lunar surface Conduct rover operations on the Moon Conduct on-site experiments on the lunar surface 1 2 3
  • 4. Key Technologies Hazard Detection and Avoidance Lander Hazard Detection & Avoidance Camera and Processing Algorithm Landing Leg Mechanism. Inertial Measurement Laser Gyro based Inertial referencing and Accelerometer package Altimeters Laser & RF based Altimeters Propulsion System 800N Throttleable Liquid Engines, 58N attitude thrusters & Throttleable Engine Control Electronics Velocimeters Laser Doppler Velocimeter & Lander Horizontal Velocity Camera Navigation, Guidance & Control Powered Descent Trajectory design and associate software elements 1 2 3 4 5 6
  • 5. Lander Special Tests Integrated Cold Test: For the demonstration of Integrated Sensors & Navigation performance test using helicopter as test platform 1 Integrated Hot test: For the demonstration of closed loop performance test with sensors, actuators and NGC using Tower crane as test platform 2 Lander Leg mechanism performance test on a lunar simulant test bed simulating different touch down conditions. 3
  • 6. Mission Components Propulsion module This module is responsible for carrying the lander and rover configuration to the Moon. It also has a scientific payload that will study the Earth from lunar orbit. Lander module This module will land on the Moon and deploy the rover. It also has a scientific payload that will study the lunar surface. Rover This is a small, mobile vehicle that will conduct on-site experiments on the lunar surface. It is equipped with a variety of scientific instruments, including a seismometer, a spectrometer, and a camera.
  • 7. Specifications For Chandrayaan-3 Sl No. Parameter Specifications Sl No. Parameter Specifications 1. Mission Life (Lander & Rover) One lunar day (~14 Earth days) 7. Communication 1.Propulsion Module: Communicates with IDSN 2.Lander Module: Communicates with IDSN and Rover. Chandrayaan-2 Orbiter is also planned for contingency link. 3.Rover: Communicates only with Lander. 2. Landing Site (Prime) 4 km x 2.4 km 69.367621 S, 32.348126 E 8. Lander Sensors 1.Laser Inertial Referencing and Accelerometer Package (LIRAP) 2.Ka-Band Altimeter (KaRA) 3.Lander Position Detection Camera (LPDC) 4.LHDAC (Lander Hazard Detection & Avoidance Camera) 5.Laser Altimeter (LASA) 6.Laser Doppler Velocimeter (LDV) 7.Lander Horizontal Velocity Camera (LHVC) 8.Micro Star sensor 9.Inclinometer & Touchdown sensors 3. Science Payloads 1.Lander:Radio Anatomy of Moon Bound Hypersensitive ionosphere and Atmosphere (RAMBHA) 2.Chandra’s Surface Thermo physical Experiment (ChaSTE) 3.Instrument for Lunar Seismic Activity (ILSA) 4.Laser Retroreflector Array (LRA) Rover: 5.Alpha Particle X-Ray Spectrometer (APXS) 6.Laser Induced Breakdown Spectroscope (LIBS) Propulsion Module: 7.Spectro-polarimetry of HAbitable Planet Earth (SHAPE) 9. Lander Actuators Reaction wheels – 4 nos (10 Nms & 0.1 Nm) 4. Two Module Configuration 1.Propulsion Module (Carries Lander from launch injection to Lunar orbit) 2.Lander Module (Rover is accommodated inside the Lander) 10. Lander Propulsion System Bi-Propellant Propulsion System (MMH + MON3), 4 nos. of 800 N Throttleable engines & 8 nos. of 58 N; Throttleable Engine Control Electronics 5. Mass 1.Propulsion Module: 2148 kg 2.Lander Module: 1752 kg including Rover of 26 kg 3.Total: 3900 kg 11. Lander Mechanisms 1.Lander leg 2.Rover Ramp (Primary & Secondary) 3.Rover 4.ILSA, Rambha & Chaste Payloads 5.Umbilical connector Protection Mechanism, 6.X- Band Antenna 6. Power generation 1.Propulsion Module: 758 W 2.Lander Module: 738W, WS with Bias 3.Rover: 50W 12. Lander Touchdown specifications 1.Vertical velocity: 2 m / sec ≤ 2.Horizontal velocity: 0.5 m / sec ≤ 3.Slope: 120 ≤
  • 8. Objectives Of Scientific Payloads SI. No Lander Payloads Objectives 1. Radio Anatomy of Moon Bound Hypersensitive ionosphere and Atmosphere (RAMBHA) Langmuir probe (LP) To measure the near surface plasma (ions and electrons) density and its changes with time 2. Chandra’s Surface Thermo physical Experiment (ChaSTE) To carry out the measurements of thermal properties of lunar surface near polar region. 3. Instrument for Lunar Seismic Activity (ILSA) To measure seismicity around the landing site and delineating the structure of the lunar crust and mantle. 4. LASER Retroreflector Array (LRA) It is a passive experiment to understand the dynamics of Moon system. SI. No Rover Payloads Objectives 1. LASER Induced Breakdown Spectroscope (LIBS) Qualitative and quantitative elemental analysis & To derive the chemical Composition and infer mineralogical composition to further our understanding of Lunar- surface. 2. Alpha Particle X-ray Spectrometer (APXS) To determine the elemental composition (Mg, Al, Si, K, Ca,Ti, Fe) of Lunar soil and rocks around the lunar landing site. Sl. No Propulsion Module Payload Objectives 1. Spectro-polarimetry of HAbitable Planet Earth (SHAPE) Future discoveries of smaller planets in reflected light would allow us to probe into variety of Exo-planets which would qualify for habitability (or for presence of life).
  • 9. Launch And Landing Of Chandrayaan-3 Chandrayaan-3 was launched on July 14, 2023. It entered a lunar transfer orbit on July 15, 2023. The lander is expected to land on the lunar south pole region on August 23 or August 24, 2023. Event Date Launch July 14, 2023 Lunar transfer orbit July 15, 2023 Landing on the lunar south pole region August 23-24, 2023
  • 10. First Indian mission to land on the lunar south pole region First Indian mission to carry a rover Advances India's space exploration capabilities Promotes international cooperation in space exploration The Significance Of Chandrayaan- 3
  • 11. Mission Life Propulsion Module 3 to 6 months 1 Lander Rover 1 Lunar Day 1 Landing Site 69.36 degree S, 32.34 degree E; slightly off the site for Chandrayaan-2 1
  • 12. Integrated Module Phase Lunar Transfer Trajectory Injectio n Orbit EBNs Lunar Orbit Insertion Lunar Orbit Lander Deboost Lander Propulsion Model Separation Touchdown Mission Profile
  • 13. Mission Profile Animation of Chandrayaan-3 Chandrayaan-3 Earth Moon
  • 14. The Earth-Moon average distance is roughly 384,400 kilometers. To save fuel, Chandrayaan-3 has chosen a longer route to the Moon. This adjusted path aims to ensure a gentle landing of the mission's Vikram lander on the Moon's South Pole area. The expected timeline for this soft touchdown is approximately 42 days after launch, specifically around August 23 or 24. Trajectory
  • 15. 01 02 03 04 05 06 07 Nominal Flight Sequence S.No Event Flight Time (s) Altitude (km) Inertial Velocity (km/s) 1 2xS200 Ignition 0.00 0.024 0.452 2 L110 Ignition 108.10 44.668 1.788 3 2xS200 Separation 127.00 62.171 1.969 4 PLF Separation 194.96 114.805 2.560 5 L110 Separation 305.56 175.352 4.623 6 C25 Ignition 307.96 176.573 4.621 7 C25 Shut-off 954.42 174.695 10.242 8 Satellite Separation 969.42 179.192 10.269
  • 16. LVM3-M4-Chandrayaan-3 Mission Timeline July 14, 2023 LVM3 M4 vehicle successfully launched Chandrayaan-3 into orbit. Chandrayaan-3, in its precise orbit, has begun its journey to the Moon. Health of the Spacecraft is normal. July 22, 2023 The fourth orbit-raising maneuver (Earth-bound perigee firing) is completed. The spacecraft is now in a 71351 km x 233 km orbit. August 06, 2023 LBN#2 is successfully completed. The spacecarft is in 170 km x 4313 km orbit around the moon July 25, 2023 Orbit-raising maneuver performed on July 25, 2023. Next firing (TransLunar Injection), is planned for August 1, 2023. July 15, 2023 The first orbit-raising maneuver (Earthbound firing-1) is successfully performed at ISTRAC/ISRO, Bengaluru. Spacecraft is now in 41762 km x 173 km orbit. July 17, 2023 The second orbit-raising maneuver performed. The spacecraft is now in 41603 km x 226 km orbit. August 05, 2023 Chandrayaan-3 is successfully inserted into the lunar orbit. The orbit achieved is 164 km x 18074 km, as intended. August 01, 2023 The spacecraft is inserted into the translunar orbit. The orbit achieved is 288 km x 369328 km. Lunar-Orbit Insertion (LOI) is planned for Aug 5, 2023.
  • 17. Chandrayaan-3 Capture First Image The Moon, as viewed by Chandrayaan-3 during Lunar Orbit Insertion
  • 18. Conclusion Of Chandrayaan 3 Chandrayaan 3 was a successful mission that achieved its objectives of soft landing on the lunar south pole region and conducting scientific experiments. The mission has furthered India's space exploration capabilities and has helped to gain a better understanding of the Moon.
  • 19. Icons
  • 20. Icons
  • 21. You can add and edit some shapes to your presentation to present your data in a visual way. ● Choose your favourite infographic and insert it in your presentation using Ctrl C + Ctrl V or Cmd C + Cmd V in Mac. ● Select one of the parts and ungroup it by right-clicking and choosing “Ungroup”. ● Change the color by clicking on the paint bucket. ● Then resize the element by clicking and dragging one of the square-shaped points of its bounding box (the cursor should look like a double-headed arrow). Remember to hold Shift while dragging to keep the proportions. ● Group the elements again by selecting them, right-clicking and choosing “Group”. ● Repeat the steps above with the other parts and when you’re done editing, copy the end result and paste it into your presentation. ● Remember to choose the “Keep source formatting” option so that it keeps the design. For more info, please visit Slideegg (Tips & Tricks). How To Edit Shapes
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