|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:aircraft_operated
|
gptkb:Soyuz
|
|
gptkbp:application
|
space launch vehicles
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:combustor_type
|
staged combustion
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
|
gptkbp:design_influence
|
modern Russian engines
|
|
gptkbp:designed_by
|
OKB-456
|
|
gptkbp:development
|
gptkb:Mikhail_Yangel
1950s
|
|
gptkbp:engine
|
gas-generator cycle
|
|
gptkbp:engine_configuration
|
vertical
clustered engine
|
|
gptkbp:engine_power
|
reliable and efficient
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:fuel_capacity
|
1.5 m
3.5 m
|
|
gptkbp:fuel_economy
|
0.5 kg/s
|
|
gptkbp:fuel_type
|
gptkb:RP-1
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-108 A engines
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:inspired_by
|
gptkb:RD-101
|
|
gptkbp:is_tested_for
|
extensive ground tests
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:legacy
|
paved the way for future engines
|
|
gptkbp:manufacturer
|
gptkb:Soviet_space_program
|
|
gptkbp:notable_mission
|
gptkb:Vostok_1
|
|
gptkbp:number_of_rooms
|
gptkb:4
6.5 MPa
|
|
gptkbp:operational_history
|
used in early space missions
|
|
gptkbp:operational_use
|
manned spaceflight
|
|
gptkbp:oxidation_states
|
gptkb:LOX
liquid oxygen
|
|
gptkbp:oxidizer_consumption
|
1.5 kg/s
|
|
gptkbp:propulsion
|
83.3
100 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:specific_impulse
|
300 seconds
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
RD-0110
|
|
gptkbp:type
|
liquid-fueled engine
|
|
gptkbp:used_in
|
gptkb:Vostok_rocket
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_MS-83
|
|
gptkbp:bfsLayer
|
5
|