|
gptkbp:instance_of
|
gptkb:naval_warfare
gptkb:Space_Launch_System
gptkb:Team_Rocket
|
|
gptkbp:adapted_into
|
different ship classes
|
|
gptkbp:allows
|
multiple missile types
|
|
gptkbp:block
|
initial configuration
upgraded configuration
future configuration
|
|
gptkbp:budget
|
$30 billion by 2025
|
|
gptkbp:budget_overruns
|
frequent
|
|
gptkbp:built
|
gptkb:Boeing
|
|
gptkbp:can_be_found_in
|
aircraft carriers
cruisers
destroyers
|
|
gptkbp:can_be_used_for
|
defensive operations
offensive operations
|
|
gptkbp:challenges
|
high
overcoming engineering hurdles
|
|
gptkbp:collaboration
|
gptkb:JAXA
gptkb:ESA
gptkb:European_Space_Agency
gptkb:CSA
yes
ESA, JAXA
|
|
gptkbp:collaborations
|
with international space agencies
|
|
gptkbp:community_engagement
|
gptkb:educational_programs
outreach programs
|
|
gptkbp:configuration
|
Block 1
Block 2
Block 1 B
|
|
gptkbp:control_system
|
fly-by-wire
digital fly-by-wire
|
|
gptkbp:crew
|
ongoing
simulator training
|
|
gptkbp:crew_capacity
|
4 astronauts
4 to 6 astronauts
up to 4 astronauts
|
|
gptkbp:critical_design_review
|
completed
|
|
gptkbp:debut
|
gptkb:Artemis_I
|
|
gptkbp:design
|
gptkb:NASA_Marshall_Space_Flight_Center
gptkb:Aerojet_Rocketdyne
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:Boeing
10 years
15 years
NASA engineers
Boeing, Northrop Grumman
block 1
|
|
gptkbp:design_features
|
modular design
|
|
gptkbp:design_purpose
|
gptkb:Mars_missions
Lunar missions
|
|
gptkbp:designed_for
|
deep space missions
launching missiles
|
|
gptkbp:developed_by
|
gptkb:United_States_Navy
gptkb:Raytheon
gptkb:NASA
the 21st century
future warfare scenarios
|
|
gptkbp:development
|
gptkb:2011
10 years
|
|
gptkbp:development_cost
|
$18 billion
estimated $18 billion
|
|
gptkbp:diameter
|
8.4 meters
|
|
gptkbp:durability
|
false
no
partially reusable
not reusable
|
|
gptkbp:enables
|
simultaneous launches
|
|
gptkbp:engine
|
gptkb:RS-25
|
|
gptkbp:engine_type
|
gptkb:RS-25
|
|
gptkbp:engineering_teams
|
collaborative efforts
|
|
gptkbp:enhances
|
combat flexibility
|
|
gptkbp:environmental_impact
|
assessed
assessed during planning
|
|
gptkbp:facilities
|
gptkb:NASA_Michoud_Assembly_Facility
gptkb:Stennis_Space_Center
|
|
gptkbp:features
|
modular design
|
|
gptkbp:first_flight
|
gptkb:Green_Run_test
gptkb:Artemis_I
gptkb:Artemis_II
gptkb:2021
gptkb:NASA_Stennis_Space_Center
2021-11-16
January 2021
November 2021
crewed
uncrewed
Green Run
validate systems
multiple ground tests
|
|
gptkbp:first_heavy_lift_launch
|
gptkb:Artemis_I
|
|
gptkbp:first_introduced
|
gptkb:1980s
|
|
gptkbp:fuel_type
|
liquid hydrogen and liquid oxygen
liquid oxygen
liquid hydrogen
|
|
gptkbp:funding
|
congressional appropriations
funded by U. S. government
|
|
gptkbp:has
|
high rate of fire
|
|
gptkbp:has_documentation
|
extensive technical manuals
|
|
gptkbp:has_height
|
98 meters
|
|
gptkbp:has_programs
|
gptkb:2011
gptkb:Artemis_program
gptkb:John_Honeycutt
|
|
gptkbp:height
|
98 meters
|
|
gptkbp:historical_significance
|
successor to Space Shuttle
Apollo program successor
first new U. S. rocket for deep space since Apollo
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Space Launch System
|
|
gptkbp:improves
|
survivability of ships
|
|
gptkbp:includes
|
launch cells
|
|
gptkbp:innovation
|
new technologies developed
|
|
gptkbp:inspiration
|
gptkb:Apollo_program
gptkb:Space_Shuttle
human space exploration
|
|
gptkbp:integration
|
gptkb:Vehicle_Assembly_Building
several months
vertical integration facility
|
|
gptkbp:involved_technology
|
gptkb:Orion_spacecraft
gptkb:advanced_propulsion_systems
|
|
gptkbp:is
|
gptkb:NASA's_heavy-lift_launch_vehicle
heavy-lift launch vehicle
|
|
gptkbp:is_based_on
|
Space Shuttle technology
|
|
gptkbp:is_compatible_with
|
NATO systems
various missile systems
|
|
gptkbp:is_considered_as
|
a force multiplier
a key asset
a technological innovation
|
|
gptkbp:is_critical_for
|
naval dominance
|
|
gptkbp:is_designed_for
|
interplanetary missions
multi-role missions
|
|
gptkbp:is_designed_to
|
gptkb:NASA's_Artemis_missions
carry crew and cargo
|
|
gptkbp:is_enhanced_by
|
advanced targeting systems
|
|
gptkbp:is_evaluated_by
|
operational readiness
cost-effectiveness
military analysts
|
|
gptkbp:is_influenced_by
|
technological advancements
|
|
gptkbp:is_integrated_with
|
gptkb:Vehicle_Assembly_Building
gptkb:combat_system
combat management systems
future naval designs
|
|
gptkbp:is_part_of
|
gptkb:NASA's_human_spaceflight_program
gptkb:Aegis_system
gptkb:Defense
gptkb:U._S._Navy_fleet
modern naval warfare
naval modernization efforts
|
|
gptkbp:is_standardized_by
|
NASA's rigorous standards
|
|
gptkbp:is_subject_to
|
international regulations
military budgets
|
|
gptkbp:is_supported_by
|
gptkb:NASA's_Space_Launch_System_program
logistics and maintenance
|
|
gptkbp:is_tested_for
|
gptkb:2020
gptkb:United_States_Navy
gptkb:B-2_Test_Stand
live-fire exercises
ground tests
uncrewed flight
|
|
gptkbp:is_used_for
|
strategic deterrence
launching asteroid missions
|
|
gptkbp:is_used_in
|
various naval platforms
|
|
gptkbp:is_used_to
|
enhance naval capabilities
|
|
gptkbp:is_utilized_in
|
joint operations
|
|
gptkbp:key_concept
|
gptkb:communication_systems
automated systems
modular design
advanced materials
ground support equipment
navigation systems
advanced avionics
environmental control systems
telemetry systems
safety systems
power systems
new propulsion systems
structural systems
launch vehicle systems
thermal protection systems
mission planning systems
sensors and instrumentation
flight software
integration systems
propellant management systems
|
|
gptkbp:launch_cadence
|
once per year
|
|
gptkbp:launch_date
|
1-2 per year
approximately 8 minutes
1-2 launches per year
1 mission per year
1 to 2 missions per year
|
|
gptkbp:launch_event
|
high success rate expected
|
|
gptkbp:launch_platform
|
gptkb:NASA's_Artemis_program
gptkb:Launch_Complex_39_B
multi-stage
mission dependent
|
|
gptkbp:launch_price
|
$2 billion per launch
estimated $2 billion per launch
estimated $2 billion
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:NASA's_heavy-lift_rockets
2
two
Ariane 5, Falcon Heavy
part of NASA's launch vehicle family
|
|
gptkbp:launch_window
|
varies by mission
|
|
gptkbp:launched
|
gptkb:Tomahawk_missiles
gptkb:Launch_Complex_39_B
gptkb:ASROC_missiles
gptkb:Kennedy_Space_Center_LC-39_B
anti-ship missiles
Standard missiles
land-attack missiles
extensive pre-launch checks
anti-air missiles
|
|
gptkbp:lifespan
|
20 years
|
|
gptkbp:local_government
|
strong
|
|
gptkbp:manufacturer
|
gptkb:NASA
|
|
gptkbp:max_thrust
|
8.8 million pounds
|
|
gptkbp:media_coverage
|
extensive
|
|
gptkbp:mission
|
gptkb:Johnson_Space_Center
gptkb:Artemis_V
gptkb:Artemis_I
gptkb:Artemis_II
gptkb:Artemis_III
gptkb:NASA_Johnson_Space_Center
gptkb:Lunar_Gateway
gptkb:Artemis_I_mission
gptkb:Artemis_IV
Artemis II, Artemis III
expected to be high
planned lunar landings
to Moon and Mars
|
|
gptkbp:mission_duration
|
varies by mission
|
|
gptkbp:mission_type
|
gptkb:uncrewed_missions
crewed missions
crewed and uncrewed missions
|
|
gptkbp:next_edition
|
gptkb:block_1_B
gptkb:block_2
|
|
gptkbp:notable_mission
|
gptkb:Artemis_program
|
|
gptkbp:number_of_stages
|
gptkb:Core_Stage
gptkb:Interim_Cryogenic_Propulsion_Stage
liquid hydrogen and liquid oxygen
liquid fuel
two stages
4 engines
|
|
gptkbp:objective
|
gptkb:Mars_exploration
|
|
gptkbp:operated_by
|
gptkb:RS-25_engines
|
|
gptkbp:operates
|
in all weather conditions
|
|
gptkbp:operational_status
|
in development
|
|
gptkbp:orbit_type
|
gptkb:Moon
|
|
gptkbp:orbital_altitude
|
7.9 km/s
7.8 km/s
28,000 km/h
up to 28,000 km/h
|
|
gptkbp:partnerships
|
gptkb:commercial_space_companies
international space agencies
|
|
gptkbp:payload_capacity
|
5 meters
yes
95 metric tons
5 meters in diameter
up to 130 metric tons
up to 130 tons
|
|
gptkbp:payload_capacity_translunar_injection
|
27 metric tons
|
|
gptkbp:primary_use
|
deep space exploration
|
|
gptkbp:project
|
gptkb:NASA's_Marshall_Space_Flight_Center
gptkb:advanced_propulsion_systems
gptkb:John_Honeycutt
return humans to the Moon
ongoing development
exploration technologies being developed
|
|
gptkbp:projected_missions
|
up to 30 missions by 2030
|
|
gptkbp:propulsion
|
8.8 million pounds
8.4 million pounds
|
|
gptkbp:provides
|
vertical launch capability
|
|
gptkbp:public_interest
|
high
|
|
gptkbp:public_perception
|
high interest and support
|
|
gptkbp:purpose
|
deep space exploration
|
|
gptkbp:reduces
|
launch preparation time
|
|
gptkbp:released
|
gptkb:Artemis_II
|
|
gptkbp:requires
|
electrical power
|
|
gptkbp:safety_features
|
gptkb:launch_escape_system
multiple redundant systems
abort system
|
|
gptkbp:safety_rating
|
high
Category 1
|
|
gptkbp:safety_record
|
ongoing assessments
|
|
gptkbp:significance
|
first heavy-lift launch since Saturn V.
|
|
gptkbp:successor
|
gptkb:Saturn_V
gptkb:Orion_spacecraft
gptkb:Space_Shuttle
gptkb:Space_X_Starship
|
|
gptkbp:support
|
gptkb:Mars_missions
|
|
gptkbp:supports
|
yes
network-centric warfare
mobile launcher
Mobile Launcher
custom designed
|
|
gptkbp:sustainability_efforts
|
ongoing
minimizing environmental footprint
|
|
gptkbp:transportation
|
gptkb:Crawler-Transporter
crawler-transporter
|
|
gptkbp:type
|
heavy-lift launch vehicle
|
|
gptkbp:upgrades
|
planned
planned for Block 2
|
|
gptkbp:used_by
|
navies
|
|
gptkbp:bfsParent
|
gptkb:The_National_Aeronautics_and_Space_Administration
gptkb:United_States_Air_Force
gptkb:National_Aeronautics_and_Space_Administration
gptkb:NASA
gptkb:Team_Rocket
|
|
gptkbp:bfsLayer
|
3
|