|
gptkbp:instance_of
|
gptkb:Mars_Rover
|
|
gptkbp:analysis
|
remote sensing
|
|
gptkbp:average_temperature
|
-40 to 50 degrees Celsius
|
|
gptkbp:chassis
|
aluminum alloy
|
|
gptkbp:collaboration
|
gptkb:none
|
|
gptkbp:collaborations
|
gptkb:international_partners
academic institutions
|
|
gptkbp:collection
|
in-situ analysis
|
|
gptkbp:communication
|
UHF band
with Vikram lander
|
|
gptkbp:communication_system
|
UHF
|
|
gptkbp:community_engagement
|
educational outreach
|
|
gptkbp:contains
|
gptkb:spectrometer
laser-induced breakdown spectroscope
|
|
gptkbp:contribution
|
enhanced understanding of lunar geology
|
|
gptkbp:control_system
|
autonomous
autonomous navigation
ground control commands
|
|
gptkbp:data_transmission
|
to Earth
to the lander
|
|
gptkbp:design_purpose
|
gptkb:Moon
|
|
gptkbp:designed_by
|
gptkb:ISRO
|
|
gptkbp:designed_for
|
gptkb:Moon
|
|
gptkbp:development
|
approximately 2 years
|
|
gptkbp:environmental_concerns
|
radiation shielding
|
|
gptkbp:first_movement_date
|
August 23, 2023
|
|
gptkbp:frequency
|
S-band
around 400 MHz
|
|
gptkbp:group_size
|
over 100 engineers
|
|
gptkbp:has_programs
|
custom-built
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Pragyan rover
|
|
gptkbp:image_processing
|
onboard processing unit
|
|
gptkbp:impact
|
contributes to future lunar exploration missions
|
|
gptkbp:instruments
|
gptkb:Alpha_Particle_X-ray_Spectrometer
Laser Induced Breakdown Spectroscopy
|
|
gptkbp:landing_site
|
gptkb:South_Pole_of_the_Moon
August 23, 2023
Moon's south pole
|
|
gptkbp:launch_date
|
July 14, 2023
|
|
gptkbp:launch_mass
|
approximately 26 kg
|
|
gptkbp:launch_site
|
gptkb:Satish_Dhawan_Space_Centre
|
|
gptkbp:launch_vehicle
|
LVM-3
|
|
gptkbp:launched
|
gptkb:Indian_Space_Research_Organisation
July 14, 2023
|
|
gptkbp:lifespan
|
one lunar day
|
|
gptkbp:max_speed
|
1 cm/s
|
|
gptkbp:mission
|
gptkb:Chandrayaan-3
analyze lunar soil
planned lunar missions
ISRO scientists
|
|
gptkbp:mission_duration
|
14 Earth days
approximately 14 Earth days
|
|
gptkbp:navigation_system
|
high precision
LIDAR
visual odometry
|
|
gptkbp:objective
|
conduct scientific experiments
demonstrate mobility on the Moon
|
|
gptkbp:operational_area
|
gptkb:lunar_south_pole
|
|
gptkbp:operational_challenges
|
extreme temperatures
lunar dust
|
|
gptkbp:operational_period
|
14 Earth days
|
|
gptkbp:operational_since
|
August 2023
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operational_use
|
lunar surface
remote commands from Earth
|
|
gptkbp:payload_capacity
|
10 kg
|
|
gptkbp:power_consumption
|
50 watts
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:provides_information_on
|
open access
|
|
gptkbp:remote_sensing_capabilities
|
yes
|
|
gptkbp:research
|
lunar surface composition
lunar topography
lunar mineralogy
lunar regolith analysis
transmitted to Earth
lunar ice detection
|
|
gptkbp:research_focus
|
lunar geology
|
|
gptkbp:research_output
|
data on lunar surface composition
|
|
gptkbp:resolution
|
high resolution
|
|
gptkbp:scientific_goals
|
search for water ice
study lunar regolith
study lunar soil
analyze mineral composition
|
|
gptkbp:scientific_instruments
|
gptkb:Alpha_Particle_X-ray_Spectrometer
gptkb:Thermal_Imaging_Camera
Laser Induced Breakdown Spectroscopy
Chandrayaan-3 Rover Payloads
|
|
gptkbp:second_movement
|
August 2023
|
|
gptkbp:storage
|
gptkb:cloud_storage
onboard memory
|
|
gptkbp:successor
|
future lunar missions
|
|
gptkbp:suspension
|
active suspension
|
|
gptkbp:sustainability
|
approximately 1.5 square meters
|
|
gptkbp:terrain
|
lunar surface
|
|
gptkbp:tire_size
|
50 cm
|
|
gptkbp:transportation
|
six wheels
tracked vehicle
|
|
gptkbp:weight
|
27 kg
26 kg
|
|
gptkbp:weight_limit
|
up to 10 kg payload
|
|
gptkbp:wheels
|
four
|
|
gptkbp:bfsParent
|
gptkb:Chandrayaan-2
|
|
gptkbp:bfsLayer
|
4
|