|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:aircraft_operated
|
8 minutes
|
|
gptkbp:block
|
Block 1
initial configuration
upgraded configuration
|
|
gptkbp:budget
|
$30 billion by 2025
|
|
gptkbp:challenges
|
complex engineering solutions required
overcoming technical hurdles
|
|
gptkbp:collaboration
|
gptkb:JAXA
gptkb:ESA
gptkb:CSA
with ESA, JAXA
|
|
gptkbp:configuration
|
multiple configurations
|
|
gptkbp:contract
|
gptkb:Boeing
|
|
gptkbp:control_system
|
advanced avionics
|
|
gptkbp:core_stage_diameter
|
8.4 meters
|
|
gptkbp:core_stage_length
|
63 meters
|
|
gptkbp:crew_capacity
|
4 astronauts
up to 4 astronauts
|
|
gptkbp:debut_year
|
gptkb:2011
|
|
gptkbp:design
|
gptkb:Boeing
gptkb:NASA's_Space_Launch_System
15 years
based on Space Shuttle technology
|
|
gptkbp:developed_by
|
gptkb:NASA
|
|
gptkbp:development
|
gptkb:NASA_Marshall_Space_Flight_Center
gptkb:2011
|
|
gptkbp:development_cost
|
estimated at $18 billion
|
|
gptkbp:diameter
|
8.4 meters
|
|
gptkbp:durability
|
not reusable
|
|
gptkbp:engine_type
|
gptkb:RS-25
|
|
gptkbp:facilities
|
gptkb:NASA's_Stennis_Space_Center
|
|
gptkbp:first_flight
|
gptkb:Green_Run_test
gptkb:Artemis_I
gptkb:Artemis_II
gptkb:2019
gptkb:2020
successful
Green Run
|
|
gptkbp:fuel_type
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:future_plans
|
Mars missions planned
|
|
gptkbp:has_programs
|
gptkb:2011
gptkb:Artemis_program
|
|
gptkbp:height
|
98 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Space Launch System (SLS)
|
|
gptkbp:infrastructure
|
Mobile Launcher
|
|
gptkbp:inspiration
|
gptkb:Apollo_program
|
|
gptkbp:integration
|
vertical integration facility
vertical integration process
|
|
gptkbp:is
|
a heavy-lift launch vehicle
|
|
gptkbp:is_a_destination_for
|
gptkb:Moon
gptkb:Mars
|
|
gptkbp:launch_date
|
1-2 launches per year
approximately once per year
|
|
gptkbp:launch_mass
|
over 2,600 metric tons
over 2.5 million kg
|
|
gptkbp:launch_platform
|
gptkb:Kennedy_Space_Center_Launch_Control_Center
gptkb:NASA_Launch_Control_Center
|
|
gptkbp:launch_price
|
estimated at $500 million
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Launch_Complex_39_B
two
heavy-lift launch vehicle
|
|
gptkbp:launch_window
|
varies by mission
specific launch windows
|
|
gptkbp:launched
|
gptkb:Launch_Complex_39_B
|
|
gptkbp:lifespan
|
20 years
|
|
gptkbp:manufacturer
|
gptkb:NASA
|
|
gptkbp:mission
|
gptkb:Johnson_Space_Center
gptkb:Artemis_I
gptkb:Artemis_III
gptkb:API
gptkb:Artemis_program
gptkb:Artemis_IV
gptkb:Mars_Sample_Return
Human exploration of Mars
Artemis II, Artemis III
Asteroid missions
Lunar South Pole missions
Lunar Gateway missions
|
|
gptkbp:mission_duration
|
varies by mission
|
|
gptkbp:mission_type
|
crewed and uncrewed
|
|
gptkbp:number_of_stages
|
four engines
ICPS
|
|
gptkbp:operational_period
|
gptkb:2022
|
|
gptkbp:orbit_type
|
gptkb:Moon
|
|
gptkbp:orbital_altitude
|
approximately 28,000 km/h
up to 28,000 km/h
|
|
gptkbp:orbital_launch
|
to be used for lunar missions
|
|
gptkbp:partnerships
|
collaborations with international space agencies
collaborations with commercial partners
|
|
gptkbp:payload_capacity
|
5 meters in diameter
up to 130 metric tons
large payload fairing
|
|
gptkbp:price
|
estimated $2 billion per launch
|
|
gptkbp:production_status
|
in development
|
|
gptkbp:projected_missions
|
multiple Artemis missions
|
|
gptkbp:public_interest
|
high public interest
|
|
gptkbp:purpose
|
deep space exploration
launch missions to the Moon and beyond
|
|
gptkbp:recovery_method
|
not applicable
|
|
gptkbp:safety_features
|
multiple redundancy systems
|
|
gptkbp:safety_measures
|
extensive testing required
|
|
gptkbp:solid_rocket_booster_diameter
|
3.7 meters
|
|
gptkbp:solid_rocket_booster_length
|
45.2 meters
|
|
gptkbp:successor
|
gptkb:Orion_spacecraft
|
|
gptkbp:supports
|
custom-built systems
specialized launch pad
|
|
gptkbp:type
|
gptkb:Team_Rocket
heavy-lift launch vehicle
|
|
gptkbp:upgrades
|
planned upgrades for Block 2
|
|
gptkbp:upper_stage_diameter
|
5 meters
|
|
gptkbp:upper_stage_height
|
15 meters
|
|
gptkbp:upper_stage_propellant
|
liquid hydrogen and liquid oxygen
|
|
gptkbp:used_for
|
gptkb:Artemis_missions
|
|
gptkbp:bfsParent
|
gptkb:NASA
|
|
gptkbp:bfsLayer
|
3
|