Mars Helicopter (Ingenuity)
GPTKB entity
Statements (130)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:helicopter
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:Perseverance_rover
|
| gptkbp:aircraft_operated |
advanced algorithms
autonomous navigation real-time adjustments several months software algorithms up to 10 meters gyroscopes technology demonstration first powered flight on another planet pre-programmed flight paths up to 5 meters per second up to 90 seconds demonstration mission new flight technologies remote commands from Earth rotors and sensors up to 3 minutes |
| gptkbp:airlines |
to Earth
to Perseverance rover |
| gptkbp:allows |
weather conditions
thin atmosphere low temperatures dust storms weather conditions on Mars |
| gptkbp:application |
gptkb:Mars_exploration
|
| gptkbp:average_temperature |
-90 to 0 degrees Celsius
|
| gptkbp:challenges |
overcome during development
design for Mars conditions |
| gptkbp:charging_time |
approximately 6 hours
|
| gptkbp:collaborates_with |
gptkb:Perseverance_rover
|
| gptkbp:collaborations |
gptkb:Jet_Propulsion_Laboratory
international partnerships |
| gptkbp:communication |
to Earth
UHF radio high-frequency radio waves via Perseverance rover direct to Earth |
| gptkbp:community_engagement |
high
|
| gptkbp:contribution |
mapping terrain
|
| gptkbp:controls |
autonomous navigation
autonomous flight |
| gptkbp:design |
gptkb:Ames_Research_Center
test flight capabilities |
| gptkbp:designed_by |
gptkb:NASA
|
| gptkbp:developer |
$80 million
|
| gptkbp:diameter |
1.2 meters
|
| gptkbp:educational_programs |
lightweight materials
|
| gptkbp:elevation |
up to 100 meters
|
| gptkbp:environmental_impact |
thin atmosphere
|
| gptkbp:features |
lightweight materials
advanced navigation system counter-rotating blades high-efficiency motors |
| gptkbp:first_flight |
gptkb:Jezero_Crater
high over 30 ongoing historic achievement successful thin atmosphere Mars atmosphere ongoing research April 19, 2021 first powered flight on another planet multiple test flights extensive simulations captured high-resolution images pre-programmed collected during missions pre-planned routes 100% in initial flights tested new technologies for future missions gyroscopic sensors 5 flights collected images developed by NASA demonstrated flight capabilities first aerial scout on Mars first in history on another planet multiple successful flights |
| gptkbp:future_plans |
further exploration missions
continue exploration missions conduct more complex flights expand flight range support Perseverance rover |
| gptkbp:height |
0.49 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mars Helicopter (Ingenuity)
|
| gptkbp:impact |
advancing aerial exploration
|
| gptkbp:inspiration |
future aerial vehicles on Mars
|
| gptkbp:instrument |
gptkb:none
gptkb:Photographer gptkb:legal_case IMU cameras and sensors thermal sensors |
| gptkbp:is_a_supporter_of |
showcasing technology
|
| gptkbp:landing_site |
gptkb:Jezero_Crater
|
| gptkbp:launched |
July 30, 2020
|
| gptkbp:max_speed |
up to 10 meters per second
|
| gptkbp:max_takeoff_weight |
gptkb:Mars
gptkb:sky_crane February 18, 2021 |
| gptkbp:media_coverage |
extensive
|
| gptkbp:mission |
gptkb:Mars_2020_mission
gptkb:Mars_2020 test flight capabilities aerial exploration planned for Mars exploration |
| gptkbp:mission_duration |
several months
up to 5 minutes |
| gptkbp:objective |
demonstrate powered flight on Mars
demonstrate powered flight |
| gptkbp:operated_by |
solar panels
|
| gptkbp:operational_area |
gptkb:Martian_atmosphere
|
| gptkbp:operational_history |
ongoing missions
|
| gptkbp:operational_status |
active
|
| gptkbp:photography |
color camera
|
| gptkbp:power_output |
solar panels
|
| gptkbp:project |
potential upgrades
|
| gptkbp:receives_funding_from |
NASA budget
|
| gptkbp:scientific_goals |
demonstrate powered flight
|
| gptkbp:storage |
onboard memory
|
| gptkbp:successor |
Mars Helicopter (Ingenuity) 2
Mars Helicopter (Ingenuity) 3 |
| gptkbp:team |
engineers and scientists
|
| gptkbp:weight |
1.8 kilograms
1.5 kilograms for payload |