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gptkbp:instance_of
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gptkb:Team_Rocket
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gptkbp:application
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gptkb:space_exploration
gptkb:Space_Launch_System
military missiles
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gptkbp:benefits
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high thrust-to-weight ratio
lack of throttle control
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gptkbp:combustor_type
|
deflagration
|
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gptkbp:components
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gptkb:Noldor
gptkb:React
gptkb:court_cases
insulation
|
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gptkbp:development
|
gptkb:Lockheed_Martin
gptkb:Northrop_Grumman
gptkb:NASA
|
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gptkbp:environmental_impact
|
produces exhaust gases
can produce noise pollution
|
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gptkbp:first_introduced
|
the 1950s
|
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gptkbp:fuel_type
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hydroxyl-terminated polybutadiene (HTPB)
aluminum powder
ammonium perchlorate
|
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gptkbp:historical_use
|
gptkb:Ares_I
gptkb:Titan_II
gptkb:Trident_missile
gptkb:Saturn_I
gptkb:Minuteman_missile
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Solid Rocket Motors
|
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gptkbp:is_tested_for
|
static fire test
cold flow test
|
|
gptkbp:key_feature
|
high reliability
quick deployment
simple storage
|
|
gptkbp:notable_examples
|
gptkb:Space_Shuttle_Solid_Rocket_Boosters
|
|
gptkbp:performance_style
|
reliability
simple design
fixed thrust
|
|
gptkbp:produced_by
|
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:project
|
advanced materials
environmentally friendly propellants
reusable systems
|
|
gptkbp:regulatory_body
|
gptkb:National_Aeronautics_and_Space_Administration_(NASA)
gptkb:Federal_Aviation_Administration_(FAA)
Department of Defense (Do D)
|
|
gptkbp:safety
|
risk of explosion
toxic propellant residues
|
|
gptkbp:used_in
|
space launch vehicles
|
|
gptkbp:uses
|
solid propellant
|
|
gptkbp:bfsParent
|
gptkb:Aero_Spire
|
|
gptkbp:bfsLayer
|
6
|