|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:application
|
launch vehicles
|
|
gptkbp:average_temperature
|
1,500 K
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:combustor_type
|
gas-generator cycle
|
|
gptkbp:control_system
|
gptkb:electronic
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:debut
|
gptkb:1964
|
|
gptkbp:designed_by
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:development
|
1950s
5 years
|
|
gptkbp:diameter
|
1.5 m
|
|
gptkbp:engine
|
staged combustion
RD series
|
|
gptkbp:engine_configuration
|
vertical
|
|
gptkbp:first_flight
|
gptkb:1966
gptkb:1980
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-0250 engine
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:is_tested_for
|
gptkb:GIK-1
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:length
|
3.5 m
|
|
gptkbp:manufacturer
|
gptkb:Kuznetsov_Design_Bureau
|
|
gptkbp:mission_type
|
orbital launch
|
|
gptkbp:number_of_rooms
|
gptkb:1
70 atm
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:propulsion
|
20:1
25,000 lbf
|
|
gptkbp:replaced_by
|
gptkb:RD-0120_engine
|
|
gptkbp:specific_impulse
|
300 seconds
|
|
gptkbp:status
|
retired
|
|
gptkbp:success_rate
|
95%
|
|
gptkbp:type
|
liquid-fueled
|
|
gptkbp:used_in
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:water_requirement
|
300 kg/s
600 kg/s
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Viktor_Mikhailovich_Glushko
|
|
gptkbp:bfsLayer
|
6
|