|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:can_be_configured_for
|
multiple mission profiles
various payload types
|
|
gptkbp:designed_for
|
deep space missions
|
|
gptkbp:developed_by
|
gptkb:NASA's_Space_Launch_System
gptkb:NASA
advanced materials
commercial partnerships
|
|
gptkbp:diameter
|
approximately 15 feet
|
|
gptkbp:enables
|
gptkb:sustainable_lunar_exploration
human exploration of Mars
|
|
gptkbp:facilitates
|
interplanetary missions
|
|
gptkbp:features
|
advanced avionics
restartable engine
|
|
gptkbp:first_flight
|
gptkb:2020
|
|
gptkbp:has
|
multiple engine restart capabilities
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Interim Cryogenic Propulsion Stage (ICPS)
|
|
gptkbp:include
|
increased payload capacity
|
|
gptkbp:is_capable_of
|
inserting payloads into orbit
|
|
gptkbp:is_compatible_with
|
multiple payload configurations
|
|
gptkbp:is_designed_for
|
high-performance missions
|
|
gptkbp:is_designed_to
|
high efficiency
deliver payloads to lunar orbit
|
|
gptkbp:is_expected_to
|
high reliability
support future lunar missions
|
|
gptkbp:is_integrated_with
|
gptkb:Orion_spacecraft
gptkb:SLS_Block_1
|
|
gptkbp:is_optimized_for
|
high-altitude operations
|
|
gptkbp:is_part_of
|
gptkb:NASA's_human_spaceflight_program
gptkb:NASA's_Artemis_missions
gptkb:NASA's_Artemis_II_mission
NASA's exploration missions
NASA's deep space exploration strategy
NASA's exploration architecture
|
|
gptkbp:is_supported_by
|
crew and cargo missions
|
|
gptkbp:is_tested_for
|
gptkb:Marshall_Space_Flight_Center
engine performance
performance metrics
simulated flight conditions
reliability and safety
|
|
gptkbp:is_used_in
|
gptkb:NASA's_Artemis_I_mission
|
|
gptkbp:launched
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:length
|
approximately 27 feet
|
|
gptkbp:mass
|
approximately 40,000 pounds
|
|
gptkbp:operates_in
|
vacuum of space
|
|
gptkbp:operational_since
|
gptkb:2020
|
|
gptkbp:propulsion
|
approximately 24,750 pounds
|
|
gptkbp:provides
|
upper stage propulsion
|
|
gptkbp:successor
|
gptkb:Delta_IV_Upper_Stage
|
|
gptkbp:support
|
gptkb:Mars_missions
|
|
gptkbp:supports
|
gptkb:Artemis_program
gptkb:NASA's_lunar_Gateway
|
|
gptkbp:used_in
|
gptkb:Space_Launch_System_(SLS)
|
|
gptkbp:uses
|
gptkb:RL10_engine
|
|
gptkbp:utilizes
|
liquid oxygen
liquid hydrogen
|
|
gptkbp:bfsParent
|
gptkb:NASA's_Space_Launch_System_(SLS)
|
|
gptkbp:bfsLayer
|
5
|