|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_FG
gptkb:RD-107
gptkb:Soyuz-2.1a
gptkb:Soyuz_MS-77
gptkb:Soyuz_2.1b
gptkb:Soyuz_2.1v
gptkb:Soyuz_2.1a
|
|
gptkbp:aircraft_operated
|
gptkb:Soyuz
|
|
gptkbp:application
|
gptkb:spacecraft
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:debut_year
|
over 100 launches
|
|
gptkbp:designed_by
|
OKB-456
|
|
gptkbp:developed_by
|
OKB-456
|
|
gptkbp:developer
|
1955-1957
|
|
gptkbp:emissions_standard
|
bell nozzle
|
|
gptkbp:engine
|
gptkb:4
gas-generator cycle
staged combustion
hypergolic
multi-chamber
four-chamber
|
|
gptkbp:engine_type
|
gptkb:rocket
liquid-fueled
RD-108, RD-109
|
|
gptkbp:features
|
modular design
|
|
gptkbp:first_flight
|
gptkb:1957
|
|
gptkbp:fuel_capacity
|
1.5 m
3.5 m
high
300 kg
|
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
staged combustion
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-107 A
|
|
gptkbp:ignition_system
|
gptkb:park
|
|
gptkbp:influenced_by
|
German rocket technology
|
|
gptkbp:inspired_by
|
gptkb:RD-101
|
|
gptkbp:is_tested_for
|
static fire tests
|
|
gptkbp:is_used_by
|
gptkb:Vostok_program
|
|
gptkbp:launch_vehicle
|
gptkb:R-7
|
|
gptkbp:legacy
|
foundation for future engines
|
|
gptkbp:manufacturer
|
gptkb:Salyut_Design_Bureau
|
|
gptkbp:mission
|
gptkb:Luna_program
|
|
gptkbp:notable_album
|
gptkb:Sputnik_1
gptkb:Vostok_1
|
|
gptkbp:notable_users
|
gptkb:Soviet_space_program
|
|
gptkbp:number_of_rooms
|
gptkb:4
single combustion chamber
6.5 M Pa
7.5 M Pa
|
|
gptkbp:operational_area
|
gptkb:spacecraft
|
|
gptkbp:operational_history
|
1957-1970
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:produced_by
|
retired
|
|
gptkbp:propulsion
|
gptkb:battle
300 seconds
100 k N
1000 k N
333:1
80:1
|
|
gptkbp:reliability
|
high
|
|
gptkbp:social_structure
|
liquid oxygen
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:RD-108
gptkb:RD-108_A
|
|
gptkbp:used_in
|
gptkb:R-7_Semyorka
|
|
gptkbp:weight
|
1,200 kg
300 kg
|