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gptkbp:instance_of
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gptkb:Team_Rocket
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|
gptkbp:aircraft_operated
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gptkb:Soyuz
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|
gptkbp:application
|
space launch vehicles
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|
gptkbp:average_temperature
|
up to 1,500 K
|
|
gptkbp:check_in_time
|
150 seconds
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|
gptkbp:combustion_chamber_material
|
gptkb:steel
|
|
gptkbp:combustor_type
|
gas-generator cycle
|
|
gptkbp:control_system
|
gptkb:manual
|
|
gptkbp:country_of_origin
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gptkb:Soviet_Union
|
|
gptkbp:designed_by
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OKB-456
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|
gptkbp:development
|
1950s
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|
gptkbp:engine
|
available in archives
controlled
open cycle
Soviet aerospace industry
influenced future designs
notable in space history
crew and cargo missions
OKB-456
ground test
used in early space missions
ongoing studies in propulsion technology
|
|
gptkbp:engine_configuration
|
staged combustion
detailed in technical manuals
|
|
gptkbp:engine_influence
|
paved the way for modern engines
|
|
gptkbp:engine_power
|
tested under various conditions
replaced by more efficient engines
|
|
gptkbp:engine_type
|
staged combustion engine
RD-108, RD-0110
|
|
gptkbp:exhaust_system
|
bell nozzle
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:fuel_capacity
|
1.5 m
3.5 m
|
|
gptkbp:fuel_economy
|
0.5 kg/s
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-108 A engine
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:is_tested_for
|
static fire test
|
|
gptkbp:number_of_rooms
|
gptkb:4
6.5 MPa
|
|
gptkbp:oxidation_states
|
liquid oxygen
|
|
gptkbp:oxidizer_consumption
|
1.5 kg/s
|
|
gptkbp:propulsion
|
83:1
100 k N
|
|
gptkbp:specific_impulse
|
300 seconds
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:RD-0110_engine
|
|
gptkbp:type
|
liquid-fueled
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|
gptkbp:used_in
|
gptkb:Vostok_rocket
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_MS-19
gptkb:Soyuz_69
gptkb:Soyuz_85
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|
gptkbp:bfsLayer
|
5
|