|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:RD-107_A_engines
|
|
gptkbp:application
|
gptkb:spacecraft
|
|
gptkbp:challenges
|
vibration control
|
|
gptkbp:check_in_time
|
150 seconds
|
|
gptkbp:collaborations
|
international space agencies
|
|
gptkbp:cooling_system
|
regenerative cooling
|
|
gptkbp:cultural_impact
|
featured in documentaries
|
|
gptkbp:debut_year
|
over 100 launches
|
|
gptkbp:designed_by
|
gptkb:Mikhail_Yangel
|
|
gptkbp:developer
|
1950s
classified
|
|
gptkbp:emissions_standard
|
bell nozzle
|
|
gptkbp:engine
|
gptkb:Yuzhnoye_Design_Office
gptkb:RD-109
gas-generator cycle
clustered
|
|
gptkbp:engine_type
|
gptkb:RD-108_A
liquid-fueled
|
|
gptkbp:environmental_impact
|
low emissions
|
|
gptkbp:first_flight
|
gptkb:1955
|
|
gptkbp:fuel_capacity
|
1.5 m
3.5 m
moderate
|
|
gptkbp:fuel_type
|
RP-1 and liquid oxygen
staged combustion
|
|
gptkbp:future_plans
|
historical studies.
|
|
gptkbp:has_documentation
|
gptkb:stock_market_index
|
|
gptkbp:historical_significance
|
first engine to launch humans into space
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RD-108 engines
|
|
gptkbp:ignition_system
|
hypergolic
|
|
gptkbp:influenced_by
|
German rocket technology
|
|
gptkbp:inspiration
|
gptkb:RD-101
|
|
gptkbp:invention
|
held by Soviet Union
|
|
gptkbp:is_tested_for
|
static fire tests
|
|
gptkbp:is_used_by
|
gptkb:Soviet_space_program
|
|
gptkbp:launch_vehicle
|
gptkb:Vostok-1
|
|
gptkbp:launched
|
gptkb:spacecraft
|
|
gptkbp:legacy
|
influenced future rocket designs
|
|
gptkbp:material
|
aluminum alloys
|
|
gptkbp:notable_album
|
gptkb:Vostok_1
|
|
gptkbp:number_of_rooms
|
four
6.5 M Pa
|
|
gptkbp:number_of_stages
|
four
|
|
gptkbp:operational_area
|
gptkb:spacecraft
20 years
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:propulsion
|
83.3
300 seconds
100 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:research_and_development
|
ongoing interest
|
|
gptkbp:retirement_year
|
1970s
|
|
gptkbp:safety_record
|
excellent
|
|
gptkbp:successor
|
RD-0110
|
|
gptkbp:used_in
|
gptkb:Vostok_rocket
|
|
gptkbp:weight
|
1,200 kg
|