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gptkbp:instance_of
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gptkb:spacecraft
|
|
gptkbp:communication_system
|
UHF radio
|
|
gptkbp:control_system
|
autonomous landing system
|
|
gptkbp:data_return
|
limited
|
|
gptkbp:dimensions
|
3.2 m x 3.2 m x 2.5 m
|
|
gptkbp:has_programs
|
Surveyor program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SURVEYOR-2
|
|
gptkbp:landing_distance
|
900 kg
|
|
gptkbp:landing_site
|
gptkb:Oceanus_Procellarum
1966-09-20
Surveyor program
|
|
gptkbp:launch_date
|
1966-04-02
|
|
gptkbp:launch_mass
|
1,000 kg
|
|
gptkbp:launch_site
|
gptkb:Cape_Canaveral
|
|
gptkbp:launch_vehicle
|
gptkb:Atlas-Centaur
|
|
gptkbp:manufacturer
|
gptkb:NASA
|
|
gptkbp:mass
|
1,000 kg
|
|
gptkbp:mission
|
crash landing
|
|
gptkbp:mission_duration
|
3 months
|
|
gptkbp:mission_type
|
gptkb:Mars_Rover
|
|
gptkbp:orbit_type
|
lunar orbit
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:predecessor
|
gptkb:SURVEYOR-1
|
|
gptkbp:research
|
chemical composition
topography
impact craters
radiation levels
surface temperature
thermal properties
seismic activity
soil composition
photometric data
spectral data
magnetic field measurements
lunar surface features
lunar soil mechanics
photographs of the lunar surface
dust properties
regolith characteristics
|
|
gptkbp:resolution
|
1 meter
|
|
gptkbp:scientific_goals
|
provide data for future missions
analyze lunar soil
test landing techniques
|
|
gptkbp:scientific_instruments
|
gptkb:spectrometer
gptkb:magnetometer
TV camera
soil scoop
|
|
gptkbp:status
|
failed
|
|
gptkbp:successor
|
gptkb:SURVEYOR-3
|
|
gptkbp:weight
|
1,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Mavyret
|
|
gptkbp:bfsLayer
|
6
|