Statements (54)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Mars_Rover
|
| gptkbp:academic_programs |
multidisciplinary team of engineers
|
| gptkbp:challenges |
landing on uneven terrain
|
| gptkbp:collaboration |
involvement with global space agencies
|
| gptkbp:collaborator |
various universities and companies
|
| gptkbp:communication_system |
high-gain antenna
|
| gptkbp:community_engagement |
educational outreach programs
|
| gptkbp:control_system |
flight control software
|
| gptkbp:cooling_system |
active thermal control system
|
| gptkbp:data_usage |
up to 1 Mbps
|
| gptkbp:design |
1 lunar day
|
| gptkbp:designed_by |
gptkb:Astrobotic_Technology
|
| gptkbp:development |
gptkb:2017
advancements in lunar landing technology |
| gptkbp:durability |
designed for multiple missions
|
| gptkbp:environmental_concerns |
thermal insulation
|
| gptkbp:features |
autonomous landing system
|
| gptkbp:first_flight |
gptkb:2023
planned for 2022 |
| gptkbp:frequency |
S-band
|
| gptkbp:funding |
private and public funding sources
|
| gptkbp:goal |
deliver payloads to the lunar surface
|
| gptkbp:home_ground |
Astrobotic's mission control
|
| https://www.w3.org/2000/01/rdf-schema#label |
Peregrine lander
|
| gptkbp:landing_distance |
soft landing
data collection and transmission |
| gptkbp:landing_precision |
within 100 meters
|
| gptkbp:landing_site |
gptkb:Moon
|
| gptkbp:launch_date |
gptkb:2023
annual missions planned |
| gptkbp:launch_site |
gptkb:Cape_Canaveral_Space_Force_Station
|
| gptkbp:launch_vehicle |
gptkb:Vulcan_Centaur
|
| gptkbp:launched |
extensive pre-launch testing
|
| gptkbp:mission |
gptkb:NASA's_Commercial_Lunar_Payload_Services
support lunar exploration evaluation of mission data planned for lunar south pole exploration successful payload delivery to the Moon |
| gptkbp:mission_duration |
approximately 14 Earth days
|
| gptkbp:mission_type |
gptkb:Moon
|
| gptkbp:navigation_system |
gptkb:navigation_system
|
| gptkbp:operational_status |
planned
|
| gptkbp:partnerships |
NASA, commercial partners
|
| gptkbp:payload_capacity |
up to 30 kg
modular payload bay scientific instruments, technology demonstrations |
| gptkbp:power_source |
solar panels
|
| gptkbp:project |
ongoing development and testing
|
| gptkbp:safety_features |
redundant systems
|
| gptkbp:scientific_instruments |
various payloads for lunar research
|
| gptkbp:sustainability_efforts |
support lunar economy
|
| gptkbp:weight |
approximately 120 kg
|
| gptkbp:bfsParent |
gptkb:Astrobotic_Technology
|
| gptkbp:bfsLayer |
4
|