|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_ST
gptkb:Soyuz-2.1c
gptkb:Soyuz-2.1e
gptkb:Soyuz-2.1g
gptkb:Soyuz-2.1i
gptkb:Soyuz-2.1k
gptkb:Soyuz-2.1m
gptkb:Soyuz-2.1s
gptkb:RD-0110_engine
gptkb:Soyuz-2
gptkb:Soyuz-2.1v
gptkb:Soyuz_2.1b
gptkb:Soyuz_2.1v
gptkb:Soyuz-2.1t
gptkb:Soyuz-2.1u
|
|
gptkbp:application
|
launch vehicles
|
|
gptkbp:average_temperature
|
-40 to 60 ° C
|
|
gptkbp:collaborations
|
limited
|
|
gptkbp:compression_ratio
|
20:1
|
|
gptkbp:controls
|
digital control system
computerized
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:designed_by
|
gptkb:Kuznetsov_Design_Bureau
|
|
gptkbp:developer
|
1990s
classified
engineers and scientists
|
|
gptkbp:diameter
|
1.5 m
|
|
gptkbp:engine
|
turbopump
single-chamber
approximately 100 flights
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:features
|
modular design
|
|
gptkbp:first_flight
|
gptkb:2004
|
|
gptkbp:fuel_capacity
|
high
|
|
gptkbp:fuel_type
|
staged combustion
kerosene
turbopump
|
|
gptkbp:future_plans
|
upgrades planned
|
|
gptkbp:historical_significance
|
important for Russian space exploration
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-0124
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:invention
|
multiple patents filed
|
|
gptkbp:is_tested_for
|
gptkb:Khrunichev_State_Research_and_Production_Space_Center
extensive ground testing
GKNP Ts im. A. M. Isaev
|
|
gptkbp:launch_site
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz_family
|
|
gptkbp:launched
|
over 50
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:manufacturer
|
gptkb:Kuznetsov
|
|
gptkbp:material
|
lightweight alloys
|
|
gptkbp:modifications
|
several iterations
|
|
gptkbp:number_of_rooms
|
90 bar
|
|
gptkbp:operational_area
|
gptkb:Russian_space_program
|
|
gptkbp:performance
|
meets mission requirements
|
|
gptkbp:propulsion
|
300 seconds
25,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:safety_record
|
excellent
|
|
gptkbp:social_structure
|
liquid oxygen
|
|
gptkbp:status
|
in service
|
|
gptkbp:successor
|
RD-0124 M
|
|
gptkbp:type
|
gptkb:rocket
|
|
gptkbp:used_in
|
gptkb:Soyuz-2_rocket
|
|
gptkbp:valve_configuration
|
solenoid valves
|
|
gptkbp:weight
|
1,200 kg
|