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gptkbp:instance_of
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gptkb:helicopter
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|
gptkbp:air_traffic_control
|
software algorithms
demonstration mission
gyroscopes and accelerometers
|
|
gptkbp:aircraft_operated
|
up to 10 meters
up to 300 meters
up to 5 meters per second
up to 90 seconds
first powered flight on Mars
|
|
gptkbp:battery_type
|
lithium-ion
|
|
gptkbp:challenges
|
design for low gravity
|
|
gptkbp:collaborations
|
gptkb:Jet_Propulsion_Laboratory
|
|
gptkbp:communication
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gptkb:radio_station
|
|
gptkbp:control_system
|
autonomous
|
|
gptkbp:cultural_impact
|
inspired future missions
|
|
gptkbp:data_transmission
|
to Perseverance rover
|
|
gptkbp:design_feature
|
counter-rotating blades
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:development
|
approximately 6 years
|
|
gptkbp:diameter
|
1.2 meters
|
|
gptkbp:elevation
|
up to 5 meters
|
|
gptkbp:first_flight
|
gptkb:Jezero_Crater
successful
thin atmosphere
April 19, 2021
collected and analyzed
100% in initial flights
|
|
gptkbp:flight_speed_record
|
up to 6 meters per second
|
|
gptkbp:flight_style
|
pre-programmed
over 50 flights
|
|
gptkbp:flight_time_record
|
up to 120 seconds
|
|
gptkbp:future_plans
|
further exploration missions
|
|
gptkbp:has_limitations
|
weather conditions
|
|
gptkbp:height
|
0.49 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Mars Helicopter Ingenuity
|
|
gptkbp:landing_distance
|
gptkb:Mars
skid landing gear
|
|
gptkbp:launched
|
July 30, 2020
|
|
gptkbp:mission_type
|
aerial exploration
|
|
gptkbp:objective
|
demonstrate powered flight on another planet
|
|
gptkbp:operational_use
|
gptkb:Martian_atmosphere
|
|
gptkbp:power_source
|
solar energy
|
|
gptkbp:public_interest
|
high
|
|
gptkbp:research_focus
|
Mars atmosphere
|
|
gptkbp:scientific_instruments
|
gptkb:none
|
|
gptkbp:successor
|
gptkb:Mars_Helicopter_Scout
|
|
gptkbp:sustainability
|
two
|
|
gptkbp:weight
|
1.8 kilograms
|
|
gptkbp:weight_limit
|
1.5 kilograms for flight
|
|
gptkbp:bfsParent
|
gptkb:NASA
|
|
gptkbp:bfsLayer
|
3
|