Statements (58)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:spacecraft
|
| gptkbp:airlines |
up to 14 days
|
| gptkbp:averageLifespan |
15 years
|
| gptkbp:capacity |
up to 4 astronauts
|
| gptkbp:collaboratedWith |
NASA
|
| gptkbp:communicationEquipment |
high-frequency radio
|
| gptkbp:crewCapacity |
up to 4 astronauts
|
| gptkbp:design |
modular design
focus on efficiency currently in development |
| gptkbp:designedBy |
gptkb:Sierra_Nevada_Corporation
|
| gptkbp:developer |
estimated at $1 billion
2020-2025 |
| gptkbp:dimensions |
9.5 m long
|
| gptkbp:electronicSystems |
comprised of aerospace experts
overcoming lunar landing dynamics |
| gptkbp:engineType |
liquid rocket engines
|
| gptkbp:environmentalImpact |
ablative heat shield
life support system |
| gptkbp:firstFlight |
2023
planned for 2024 |
| gptkbp:hasArea |
NASA_facilities
|
| gptkbp:hasFunding |
government and private investment
|
| https://www.w3.org/2000/01/rdf-schema#label |
Dream Chaser Lunar Lander
|
| gptkbp:inspiration |
Space Shuttle
|
| gptkbp:internationalCooperation |
involvement_with_ESA
|
| gptkbp:keyIssues |
successful test flights
|
| gptkbp:landingGear |
vertical landing
|
| gptkbp:launched |
2025-2030
annual missions planned |
| gptkbp:launchSite |
gptkb:Cape_Canaveral
|
| gptkbp:launchVehicle |
Atlas V
|
| gptkbp:mission |
cargo and crew missions
|
| gptkbp:navigationEquipment |
autonomous navigation
|
| gptkbp:operatedBy |
2025
|
| gptkbp:operationalRole |
support lunar base construction
|
| gptkbp:partnerships |
commercial space companies
|
| gptkbp:partOf |
Dream Chaser family
|
| gptkbp:passenger_traffic |
scientific instruments
|
| gptkbp:passengerCapacity |
up to 1,000 kg
|
| gptkbp:powers |
solar panels
|
| gptkbp:products |
gptkb:NASA_Artemis_program
|
| gptkbp:project |
2025
$1 billion advancing space exploration |
| gptkbp:publicAccess |
high due to lunar exploration
|
| gptkbp:purpose |
lunar exploration
|
| gptkbp:reliability |
fully reusable
|
| gptkbp:respondsTo |
splashdown
|
| gptkbp:safetyFeatures |
ongoing
redundant systems |
| gptkbp:scientificName |
sample return missions
|
| gptkbp:secondaryMission |
Mars_missions_planned
|
| gptkbp:sustainability |
green technologies
|
| gptkbp:targets |
lunar south pole
|
| gptkbp:technology |
advanced robotics
in-situ resource utilization |
| gptkbp:weight |
approximately 10,000 kg
|