Statements (52)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:helicopter
|
| gptkbp:bfsLayer |
3
|
| gptkbp:bfsParent |
gptkb:Neil_Armstrong
gptkb:NASA |
| gptkbp:aircraft_operated |
software algorithms
up to 10 meters up to 300 meters up to 5 meters per second up to 90 seconds demonstration mission first powered flight on Mars gyroscopes and accelerometers |
| gptkbp:allows |
weather conditions
|
| gptkbp:battery_life |
lithium-ion
|
| gptkbp:challenges |
design for low gravity
|
| gptkbp:collaborations |
gptkb:Jet_Propulsion_Laboratory
|
| gptkbp:communication |
gptkb:aircraft
to Perseverance rover |
| gptkbp:community_engagement |
high
|
| gptkbp:controls |
autonomous
|
| gptkbp:cultural_impact |
inspired future missions
|
| gptkbp:designed_by |
gptkb:NASA
|
| gptkbp:developer |
approximately 6 years
|
| gptkbp:diameter |
1.2 meters
|
| gptkbp:elevation |
up to 5 meters
|
| gptkbp:features |
counter-rotating blades
|
| gptkbp:first_flight |
gptkb:Jezero_Crater
successful thin atmosphere April 19, 2021 pre-programmed collected and analyzed 100% in initial flights over 50 flights up to 120 seconds |
| gptkbp:future_plans |
further exploration missions
|
| gptkbp:height |
0.49 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mars Helicopter Ingenuity
|
| gptkbp:instrument |
gptkb:none
|
| gptkbp:launched |
July 30, 2020
|
| gptkbp:max_takeoff_weight |
gptkb:Mars
skid landing gear |
| gptkbp:mission |
aerial exploration
|
| gptkbp:objective |
demonstrate powered flight on another planet
|
| gptkbp:operational_area |
gptkb:Martian_atmosphere
|
| gptkbp:power_output |
solar energy
|
| gptkbp:research_focus |
Mars atmosphere
|
| gptkbp:speed |
up to 6 meters per second
|
| gptkbp:successor |
gptkb:Mars_Helicopter_Scout
|
| gptkbp:sustainability |
two
|
| gptkbp:weight |
1.8 kilograms
1.5 kilograms for flight |