|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
launch vehicles
|
|
gptkbp:average_temperature
|
up to 3000 K
|
|
gptkbp:cargo_capacity
|
500 kg
|
|
gptkbp:combustor_type
|
gas-generator cycle
|
|
gptkbp:control_system
|
digital
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:crew_capacity
|
gptkb:3
|
|
gptkbp:designed_by
|
gptkb:Kuznetsov_Design_Bureau
|
|
gptkbp:development
|
1970s
|
|
gptkbp:development_cost
|
classified
|
|
gptkbp:diameter
|
1.5 m
|
|
gptkbp:durability
|
not reusable
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
staged combustion
|
|
gptkbp:engine_configuration
|
fixed mount
|
|
gptkbp:environment
|
gptkb:space
|
|
gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:fuel_economy
|
0.5 kg/s
|
|
gptkbp:fuel_type
|
gptkb:tank
kerosene
|
|
gptkbp:historical_significance
|
important in space exploration
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-0240 engine
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:is_tested_for
|
GIK-112
|
|
gptkbp:launch_date
|
monthly
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:legacy
|
influenced future designs
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:manufacturer
|
gptkb:Kuznetsov
|
|
gptkbp:mission_duration
|
up to 10 days
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:notable_launches
|
gptkb:Soyuz_missions
|
|
gptkbp:number_of_rooms
|
gptkb:1
8 MPa
|
|
gptkbp:operational_use
|
crew and cargo missions
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:oxidizer_consumption
|
1.0 kg/s
|
|
gptkbp:oxidizer_storage
|
gptkb:tank
|
|
gptkbp:propulsion
|
0.3
240 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:safety_record
|
excellent
|
|
gptkbp:specific_impulse
|
300 seconds
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
RD-0124 engine
|
|
gptkbp:used_in
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:user_countries
|
limited
|
|
gptkbp:valve_configuration
|
solenoid
|
|
gptkbp:vibration_damping
|
active system
|
|
gptkbp:weight
|
800 kg
|
|
gptkbp:bfsParent
|
gptkb:Viktor_Mikhailovich_Glushko
|
|
gptkbp:bfsLayer
|
6
|