|
gptkbp:instance_of
|
gptkb:spacecraft
gptkb:gasoline
|
|
gptkbp:associated_with
|
gptkb:NASA
|
|
gptkbp:capacity
|
1,500,000 liters
|
|
gptkbp:challenges
|
Thermal protection during ascent
|
|
gptkbp:color
|
gptkb:orange
|
|
gptkbp:cooling_system
|
Foam insulation
|
|
gptkbp:decommissioned
|
gptkb:2011
|
|
gptkbp:design
|
Cylindrical
10 missions
|
|
gptkbp:designed_by
|
gptkb:NASA
|
|
gptkbp:development
|
1970s
|
|
gptkbp:diameter
|
8.4 meters
|
|
gptkbp:discontinued
|
gptkb:2011
|
|
gptkbp:environmental_impact
|
Ocean pollution
|
|
gptkbp:exterior_features
|
foam insulation
Spray-on Foam Insulation
|
|
gptkbp:first_flight
|
gptkb:STS-1
gptkb:STS-135
|
|
gptkbp:fuel_capacity
|
1,000,000 liters of Liquid Hydrogen
500,000 liters of Liquid Oxygen
|
|
gptkbp:fuel_type
|
Liquid Oxygen and Liquid Hydrogen
|
|
gptkbp:function
|
Fuel storage
store propellant
|
|
gptkbp:has_units
|
135
|
|
gptkbp:height
|
46.8 meters
46.0 meters
|
|
gptkbp:historical_significance
|
First large-scale use of external tanks
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
External Tank
|
|
gptkbp:integration
|
Vertical Integration Facility
|
|
gptkbp:investment
|
0.5 bar
|
|
gptkbp:launch_mass
|
1,500,000 kg
|
|
gptkbp:launch_site
|
gptkb:Kennedy_Space_Center
|
|
gptkbp:launch_vehicle
|
gptkb:Space_Shuttle
|
|
gptkbp:launched
|
135
Ground support equipment
|
|
gptkbp:legacy
|
Foundation for future launch systems
|
|
gptkbp:length
|
46.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Rockwell_International
|
|
gptkbp:mass
|
36,000 kg
|
|
gptkbp:material
|
aluminum
|
|
gptkbp:mission
|
gptkb:STS-135
Various Space Shuttle missions
|
|
gptkbp:modifications
|
Various design iterations
|
|
gptkbp:operational_period
|
1981 to 2011
|
|
gptkbp:operational_use
|
gptkb:Space_Launch_System
|
|
gptkbp:payload_capacity
|
27,000 kg to Low Earth Orbit
|
|
gptkbp:production_location
|
gptkb:Michoud_Assembly_Facility
|
|
gptkbp:propulsion
|
0 N
|
|
gptkbp:replaced_by
|
gptkb:Core_Stage_of_Space_Launch_System
gptkb:SLS_Core_Stage
|
|
gptkbp:safety_features
|
Pressure relief valves
|
|
gptkbp:support
|
Launch support
|
|
gptkbp:supporting_structure
|
gptkb:Solid_Rocket_Boosters
|
|
gptkbp:transportation
|
gptkb:boat
|
|
gptkbp:used_by
|
gptkb:Space_Shuttle
|
|
gptkbp:used_for
|
Transporting propellants
|
|
gptkbp:used_in
|
gptkb:Space_Shuttle
|
|
gptkbp:venting_system
|
Gaseous Hydrogen Venting System
|
|
gptkbp:waste_management
|
Ocean disposal
|
|
gptkbp:weight
|
36,000 kg
29,000 kg
|
|
gptkbp:bfsParent
|
gptkb:Space_Shuttle
|
|
gptkbp:bfsLayer
|
4
|