|
gptkbp:instance_of
|
gptkb:Mars_Rover
|
|
gptkbp:acceleration
|
30 degrees
|
|
gptkbp:color
|
gptkb:White
|
|
gptkbp:communication_system
|
gptkb:radio_station
|
|
gptkbp:control_system
|
gptkb:remote_control
|
|
gptkbp:crew_capacity
|
2 astronauts
|
|
gptkbp:deployment
|
Foldable
|
|
gptkbp:design
|
3 lunar days
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:development
|
1960s
|
|
gptkbp:emergency_services
|
gptkb:Hadley-Apennine
gptkb:Taurus-Littrow
|
|
gptkbp:first_introduced
|
gptkb:1971
|
|
gptkbp:has_units
|
gptkb:3
|
|
gptkbp:historical_significance
|
First rovers on the Moon
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Apollo Lunar Rover
|
|
gptkbp:inspiration
|
Future lunar rovers
|
|
gptkbp:landing_site
|
gptkb:Moon
|
|
gptkbp:launch_date
|
1971-07-26
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Saturn_V
|
|
gptkbp:legacy
|
Pioneered lunar exploration
|
|
gptkbp:manufacturer
|
gptkb:Grumman_Aircraft_Engineering_Corporation
|
|
gptkbp:max_speed
|
13 km/h
|
|
gptkbp:mission
|
gptkb:Apollo_16
gptkb:Apollo_15
gptkb:Apollo_17
|
|
gptkbp:navigation_system
|
Inertial navigation
|
|
gptkbp:operational_cost
|
Not disclosed
|
|
gptkbp:operational_period
|
3 days
|
|
gptkbp:operational_range
|
92 km
|
|
gptkbp:operational_status
|
Retired
|
|
gptkbp:operational_use
|
Lunar environment
|
|
gptkbp:payload_capacity
|
500 kg
|
|
gptkbp:power_source
|
gptkb:battery
|
|
gptkbp:primary_function
|
gptkb:transportation
Scientific exploration
|
|
gptkbp:related_vehicle
|
gptkb:Mars_Rover
|
|
gptkbp:scientific_goals
|
Sample collection
|
|
gptkbp:scientific_instruments
|
Geology tools
|
|
gptkbp:seating_capacity
|
2
|
|
gptkbp:service
|
gptkb:1972
|
|
gptkbp:suspension
|
Independent suspension
|
|
gptkbp:terrain
|
gptkb:High
Lunar surface
|
|
gptkbp:tire_size
|
gptkb:4
32 inches
|
|
gptkbp:weight
|
210 kg
|
|
gptkbp:weight_limit
|
400 kg
|
|
gptkbp:bfsParent
|
gptkb:NASA
|
|
gptkbp:bfsLayer
|
3
|