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gptkbp:instance_of
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gptkb:chemical_compound
gptkb:Team_Rocket
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gptkbp:academic_programs
|
used as a case study
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gptkbp:application
|
launch vehicles
potential in new rockets
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|
gptkbp:benefits
|
successful engine development.
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gptkbp:casnumber
|
123456-78-9
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gptkbp:challenges
|
overheating issues
|
|
gptkbp:check_in_time
|
150 seconds
|
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gptkbp:chemical_formula
|
C12 H15 N3 O2
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|
gptkbp:collaboration
|
with other space agencies
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|
gptkbp:collaborative_projects
|
with universities
|
|
gptkbp:component_testing
|
rigorous testing protocols
|
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gptkbp:composed_by
|
gptkb:chemical_compound
|
|
gptkbp:conference
|
presented at aerospace conferences
|
|
gptkbp:control_system
|
electronic control
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:design
|
applied in design
multiple iterations before final version
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:designed_by
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:development
|
1960s
engineers at Kuznetsov
|
|
gptkbp:economic_impact
|
gptkb:significant
|
|
gptkbp:engine
|
staged combustion
|
|
gptkbp:engine_configuration
|
vertical
|
|
gptkbp:environmental_impact
|
low
|
|
gptkbp:exhaust_system
|
bell nozzle
|
|
gptkbp:first_flight
|
gptkb:1966
|
|
gptkbp:fuel_economy
|
moderate
|
|
gptkbp:fuel_type
|
gptkb:RP-1
|
|
gptkbp:funding
|
government funded
|
|
gptkbp:future_prospects
|
gptkb:advanced_propulsion_systems
|
|
gptkbp:has_documentation
|
available for study
|
|
gptkbp:historical_significance
|
important in space exploration
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-0214
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:improves
|
implemented over time
|
|
gptkbp:invention
|
held by Kuznetsov
|
|
gptkbp:is_standardized_by
|
met industry standards
|
|
gptkbp:is_tested_for
|
gptkb:Gromov_Flight_Research_Institute
extensive ground testing
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:legacy
|
influenced future engine designs
|
|
gptkbp:manufacturer
|
gptkb:Kuznetsov_Design_Bureau
|
|
gptkbp:material
|
aluminum and titanium
|
|
gptkbp:notable_users
|
gptkb:Soviet_Union
|
|
gptkbp:number_of_rooms
|
single chamber
8 MPa
|
|
gptkbp:operational_history
|
used in multiple missions
|
|
gptkbp:operational_use
|
gptkb:Soviet_space_program
|
|
gptkbp:oxidation_states
|
gptkb:LOX
|
|
gptkbp:part_of
|
Russian space heritage
|
|
gptkbp:performance
|
evaluated during tests
|
|
gptkbp:previous_name
|
N-(4-(4-(dimethylamino)phenyl)-6-methylpyrimidin-2-yl)acetamide
|
|
gptkbp:production_status
|
gptkb:Clinical_Trials
|
|
gptkbp:project
|
managed by experienced teams
achieve reliable launch capabilities
completed in a decade
|
|
gptkbp:propulsion
|
kerosene and liquid oxygen
100 k N
|
|
gptkbp:publications
|
numerous technical papers
|
|
gptkbp:related_to
|
mental health
|
|
gptkbp:reliability
|
high
|
|
gptkbp:research_and_development
|
ongoing improvements
|
|
gptkbp:retirement_year
|
gptkb:1990
|
|
gptkbp:safety_record
|
good
|
|
gptkbp:specific_impulse
|
300 seconds
|
|
gptkbp:specification
|
documented in manuals
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:RD-0213
|
|
gptkbp:targets
|
gptkb:depression
|
|
gptkbp:training_programs
|
for engineers
|
|
gptkbp:type
|
liquid-fueled engine
|
|
gptkbp:used_in
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:uses
|
gptkb:depression
|
|
gptkbp:weight
|
200 kg
233.27 g/mol
|