|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:components
|
gptkb:gasoline
valves
fuel tanks
|
|
gptkbp:composed_of
|
multiple thrusters
|
|
gptkbp:control_system
|
spacecraft orientation
|
|
gptkbp:designed_for
|
gptkb:Orion_spacecraft
|
|
gptkbp:developed_by
|
gptkb:advanced_technology
gptkb:Lockheed_Martin
NASA contracts
|
|
gptkbp:enables
|
deep space missions
|
|
gptkbp:enhances
|
mission flexibility
|
|
gptkbp:features
|
redundant systems
|
|
gptkbp:first_introduced
|
gptkb:Artemis_I_mission
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Service Propulsion System
|
|
gptkbp:includes
|
reaction control system
main engine
|
|
gptkbp:is_capable_of
|
in-space maneuvers
|
|
gptkbp:is_compatible_with
|
various launch vehicles
|
|
gptkbp:is_critical_for
|
gptkb:mission_success
|
|
gptkbp:is_designed_to
|
minimize risks
support human exploration
enable sustainable exploration
|
|
gptkbp:is_evaluated_by
|
efficiency
NASA engineers
|
|
gptkbp:is_integrated_with
|
gptkb:Orion_Multi-Purpose_Crew_Vehicle
navigation systems
|
|
gptkbp:is_monitored_by
|
flight control team
|
|
gptkbp:is_optimized_for
|
gptkb:performance
|
|
gptkbp:is_part_of
|
gptkb:NASA's_Artemis_program
gptkb:Orion_program
space exploration initiatives
|
|
gptkbp:is_subject_to
|
gptkb:regulations
|
|
gptkbp:is_tested_for
|
reliability
safety
aerospace engineers
vacuum conditions
|
|
gptkbp:is_used_for
|
spacecraft docking
orbital insertion
landing operations
deorbit maneuvers
trajectory correction
|
|
gptkbp:is_used_in
|
gptkb:Mars_missions
lunar missions
crew exploration missions
|
|
gptkbp:operates
|
liquid propellant
|
|
gptkbp:operates_under
|
various altitudes
|
|
gptkbp:operational_since
|
gptkb:2020
|
|
gptkbp:provides
|
thrust
attitude control
|
|
gptkbp:requires
|
ground support equipment
|
|
gptkbp:supports
|
crew safety
|
|
gptkbp:used_by
|
gptkb:NASA
|
|
gptkbp:utilizes
|
hypergolic propellants
|
|
gptkbp:bfsParent
|
gptkb:Apollo_Service_Module
|
|
gptkbp:bfsLayer
|
5
|