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gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
gptkb:Space_Launch_System
|
|
gptkbp:assembly_location
|
Aerojet Rocketdyne facilities
|
|
gptkbp:average_temperature
|
up to 1,500 K
|
|
gptkbp:check_in_time
|
approximately 150 seconds
|
|
gptkbp:collaboration
|
various aerospace companies
joint projects with other countries
|
|
gptkbp:combustor_type
|
gas-generator cycle
|
|
gptkbp:community_engagement
|
outreach programs for students
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:design
|
10 years
|
|
gptkbp:designed_by
|
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:development
|
gptkb:NASA
|
|
gptkbp:development_cost
|
millions of dollars
|
|
gptkbp:educational_use
|
case studies in engineering programs
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:exhaust_system
|
bell nozzle
|
|
gptkbp:first_flight
|
2000s
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
cryogenic tanks
RP-1 and liquid oxygen
|
|
gptkbp:has_documentation
|
technical manuals available
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-0146 engine
|
|
gptkbp:ignition_system
|
gptkb:spark_plug
|
|
gptkbp:inspired_by
|
previous rocket engines
|
|
gptkbp:invention
|
multiple patents filed
|
|
gptkbp:is_tested_for
|
developmental testing
NASA test facilities
|
|
gptkbp:launched
|
over 50 launches
|
|
gptkbp:legacy
|
influenced future designs
|
|
gptkbp:manufacturer
|
gptkb:Aerojet_Rocketdyne
|
|
gptkbp:material
|
high-strength alloys
|
|
gptkbp:number_of_rooms
|
approximately 300 psi
|
|
gptkbp:operational_status
|
gptkb:historical_significance
|
|
gptkbp:operational_use
|
military and commercial
|
|
gptkbp:part_of
|
gptkb:Team_Rocket
|
|
gptkbp:performance
|
reliable
|
|
gptkbp:propulsion
|
approximately 100,000 lbf
|
|
gptkbp:publications
|
numerous research papers
|
|
gptkbp:related_to
|
gptkb:Space_Shuttle
|
|
gptkbp:research_and_development
|
ongoing improvements
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:specific_impulse
|
approximately 300 seconds
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:RD-0147_engine
|
|
gptkbp:trends
|
advancements in propulsion technology
|
|
gptkbp:type
|
gptkb:Team_Rocket
|
|
gptkbp:used_in
|
launch vehicles
|
|
gptkbp:valve_configuration
|
solenoid valves
|
|
gptkbp:weight
|
approximately 1,500 lbs
|
|
gptkbp:bfsParent
|
gptkb:Viktor_Mikhailovich_Glushko
|
|
gptkbp:bfsLayer
|
6
|