|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
gptkb:Space_Launch_System
|
|
gptkbp:challenges
|
gptkb:overcome
|
|
gptkbp:check_in_time
|
150 s
|
|
gptkbp:collaboration
|
limited
|
|
gptkbp:combustor_type
|
gptkb:liquid
|
|
gptkbp:contribution
|
to rocketry
|
|
gptkbp:control_system
|
gptkb:electronic
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:design
|
10 years
|
|
gptkbp:design_features
|
innovative
|
|
gptkbp:development
|
gptkb:Soviet_Union
5 years
RD
|
|
gptkbp:engine
|
staged combustion
|
|
gptkbp:engine_configuration
|
gptkb:single
|
|
gptkbp:engine_power
|
evaluated
|
|
gptkbp:environment
|
gptkb:space
|
|
gptkbp:environmental_impact
|
assessed
|
|
gptkbp:exhaust_system
|
bell nozzle
|
|
gptkbp:first_flight
|
gptkb:20
1960s
|
|
gptkbp:fuel_capacity
|
1.5 m
3.0 m
|
|
gptkbp:fuel_economy
|
optimized
0.5 kg/s
|
|
gptkbp:fuel_tank
|
integrated
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:has_publications
|
published
|
|
gptkbp:historical_context
|
Cold War era
|
|
gptkbp:historical_significance
|
early space exploration
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RDS-37
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:influence
|
on modern engines
|
|
gptkbp:invention
|
held by RD
|
|
gptkbp:is_tested_for
|
gptkb:Moscow
conducted
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz
|
|
gptkbp:legacy
|
influenced future designs
|
|
gptkbp:manufacturer
|
RD
|
|
gptkbp:material
|
advanced alloys
|
|
gptkbp:notable_mission
|
various satellite launches
|
|
gptkbp:number_of_rooms
|
60 bar
|
|
gptkbp:operational_history
|
successful
|
|
gptkbp:operational_use
|
1970s
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:oxidizer_consumption
|
1.0 kg/s
|
|
gptkbp:oxidizer_efficiency
|
optimized
|
|
gptkbp:oxidizer_tank
|
integrated
|
|
gptkbp:project
|
inspired.
|
|
gptkbp:propulsion
|
185
37 k N
|
|
gptkbp:publications
|
numerous
|
|
gptkbp:reliability
|
high
|
|
gptkbp:replaced_by
|
newer models
|
|
gptkbp:retirement
|
technological advancement
|
|
gptkbp:safety_measures
|
implemented
|
|
gptkbp:specific_impulse
|
300 s
|
|
gptkbp:specification
|
available
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:RD-0120
|
|
gptkbp:used_in
|
gptkb:spacecraft
|
|
gptkbp:weight
|
200 kg
|
|
gptkbp:bfsParent
|
gptkb:Soviet_nuclear_designs
gptkb:The_Luna_Bomb
|
|
gptkbp:bfsLayer
|
6
|