Statements (104)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Mars_Rover
|
| gptkbp:academic_programs |
team of engineers and scientists
comprised of experienced aerospace engineers |
| gptkbp:budget |
estimated at $2 billion
estimated cost of development |
| gptkbp:cargo_capacity |
up to 3,600 kg to lunar surface
|
| gptkbp:challenges |
overcoming engineering challenges for lunar landing
overcoming lunar dust issues |
| gptkbp:collaboration |
gptkb:NASA
collaborations with other space agencies potential partnerships with other space agencies |
| gptkbp:communication_system |
high-gain antenna
high-bandwidth data link |
| gptkbp:community_engagement |
engaging with the space community
|
| gptkbp:community_outreach |
educational outreach programs planned
|
| gptkbp:crew_capacity |
up to 4 astronauts
|
| gptkbp:design |
conceptual design phase
|
| gptkbp:design_feature |
modular architecture
|
| gptkbp:design_purpose |
sustainability for long-term lunar presence
|
| gptkbp:designed_by |
gptkb:Blue_Origin
|
| gptkbp:designed_for |
lunar missions
|
| gptkbp:developed_by |
gptkb:Blue_Origin
|
| gptkbp:diameter |
approximately 4 meters
|
| gptkbp:durability |
designed for multiple missions
|
| gptkbp:elevation |
up to 100 kilometers
|
| gptkbp:environmental_concerns |
thermal protection system
|
| gptkbp:environmental_impact |
assessing environmental impact of missions
conducted at Blue Origin facilities |
| gptkbp:facilities |
utilizing advanced test facilities
|
| gptkbp:first_flight |
planned for 2023
planned test flights planned for mid-2020s |
| gptkbp:first_uncrewed_launch |
2024
|
| gptkbp:fuel_type |
cryogenic propellants
|
| gptkbp:funding |
funded through public and private sources
partially funded by government contracts |
| gptkbp:future_plans |
support lunar base development
|
| gptkbp:future_prospects |
sustained lunar presence
|
| gptkbp:has_ability |
deliver science payloads
|
| gptkbp:has_programs |
gptkb:NASA's_Artemis_program
gptkb:Artemis_program |
| gptkbp:height |
approximately 5 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Blue Moon lander
|
| gptkbp:innovation |
focus on innovative engineering solutions
focus on technological innovation for space exploration |
| gptkbp:inspiration |
inspire future generations of explorers
inspired by previous lunar missions |
| gptkbp:integrates_with |
gptkb:Gateway_lunar_station
|
| gptkbp:is_a_supporter_of |
public demonstrations of technology
planned public demonstrations of capabilities |
| gptkbp:is_capable_of |
carrying crew
delivering payloads |
| gptkbp:is_explored_in |
future exploration of the solar system
|
| gptkbp:is_tested_for |
conduct operational testing on Earth
|
| gptkbp:landing_distance |
soft landing
four landing legs |
| gptkbp:landing_site |
gptkb:lunar_south_pole
|
| gptkbp:launch_site |
gptkb:Cape_Canaveral_Space_Force_Station
|
| gptkbp:launch_vehicle |
gptkb:New_Glenn
|
| gptkbp:launch_window |
2020s
|
| gptkbp:manufacturer |
gptkb:Blue_Origin
|
| gptkbp:marketed_as |
potential commercial applications in lunar economy
|
| gptkbp:mass |
approximately 3,600 kg
|
| gptkbp:mission |
scientific research and exploration
achieve sustainable lunar exploration support future Mars missions future missions to Mars and beyond |
| gptkbp:mission_duration |
up to 14 days
|
| gptkbp:mission_type |
cargo and crew missions
|
| gptkbp:navigation_system |
gptkb:navigation_system
autonomous navigation |
| gptkbp:partnerships |
collaborations with private sector
engaging with commercial partners |
| gptkbp:payload_capacity |
up to 6,500 kg
up to 6.5 metric tons |
| gptkbp:power_source |
solar panels
|
| gptkbp:production_status |
in development
|
| gptkbp:project |
managed by experienced project managers
project timeline for development and testing on schedule for initial launch |
| gptkbp:propulsion |
liquid oxygen and liquid hydrogen
liquid oxygen and hydrogen |
| gptkbp:public_interest |
high public interest
high interest in lunar exploration |
| gptkbp:purpose |
gptkb:Moon
|
| gptkbp:regulatory_compliance |
requires regulatory approval for launches
|
| gptkbp:reviews |
completed preliminary design review
|
| gptkbp:risk_management |
comprehensive risk management strategies
|
| gptkbp:safety_features |
redundant systems
|
| gptkbp:safety_measures |
extensive safety testing planned
|
| gptkbp:scientific_instruments |
various payloads
various scientific payloads |
| gptkbp:supply_chain |
developing a robust supply chain
|
| gptkbp:support |
support lunar Gateway
|
| gptkbp:surface |
conduct surface operations on the Moon
|
| gptkbp:sustainability |
utilizing lunar resources
|
| gptkbp:sustainability_features |
reusable components
|
| gptkbp:targets |
gptkb:Artemis_program
|
| gptkbp:unveiled_on |
gptkb:2019
|
| gptkbp:was_a_demonstration_of |
demonstrate lunar landing technologies
demonstrate new technologies for lunar missions |
| gptkbp:weight |
approximately 15,000 kg
|
| gptkbp:bfsParent |
gptkb:Blue_Origin
|
| gptkbp:bfsLayer |
4
|