|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
3
|
|
gptkbp:bfsParent
|
gptkb:spacecraft
|
|
gptkbp:application
|
gptkb:Soviet_space_program
space launch vehicles
|
|
gptkbp:check_in_time
|
300 seconds
150 s
|
|
gptkbp:controls
|
gptkb:electronic
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:designed_by
|
OKB-456
|
|
gptkbp:developer
|
gptkb:Monarch
|
|
gptkbp:emissions_standard
|
converging-diverging
|
|
gptkbp:engine
|
vertical
gas-generator cycle
multi-chamber
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:fuel_type
|
gptkb:RP-1
staged combustion
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-108 engine
|
|
gptkbp:inspired
|
gptkb:RD-180
|
|
gptkbp:launch_vehicle
|
R-7 rocket
|
|
gptkbp:manufacturer
|
gptkb:Khrunichev_State_Research_and_Production_Space_Center
|
|
gptkbp:notable_album
|
gptkb:Vostok_1
|
|
gptkbp:number_of_rooms
|
gptkb:4
gptkb:5
gptkb:single
6.5 M Pa
|
|
gptkbp:operational_area
|
1960s
|
|
gptkbp:produced_by
|
retired
|
|
gptkbp:propulsion
|
83.3
300 s
100 k N
150 k N
305 s
|
|
gptkbp:reliability
|
high
|
|
gptkbp:social_structure
|
gptkb:LOX
liquid oxygen
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:RD-180
RD-0110
|
|
gptkbp:type
|
liquid-fueled
|
|
gptkbp:used_in
|
gptkb:Vostok_rocket
gptkb:Vostok_spacecraft
|
|
gptkbp:weight
|
1,200 kg
1,500 kg
|