|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:associated_with
|
gptkb:Yuri_Gagarin
|
|
gptkbp:controls
|
inertial guidance
|
|
gptkbp:country
|
gptkb:Monarch
|
|
gptkbp:decommissioned
|
gptkb:1960
|
|
gptkbp:developer
|
gptkb:1955
gptkb:1957
|
|
gptkbp:diameter
|
3.0 m
|
|
gptkbp:durability
|
gptkb:battle
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:first_flight
|
1957-09-04
|
|
gptkbp:historical_significance
|
gptkb:first_intercontinental_ballistic_missile
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
R-7 A Semyorka
|
|
gptkbp:influenced
|
future rocket designs
|
|
gptkbp:influenced_by
|
gptkb:battle
German rocket technology
|
|
gptkbp:inspiration
|
gptkb:Vostok_program
|
|
gptkbp:inspired_by
|
gptkb:V-2_rocket
|
|
gptkbp:is_explored_in
|
gptkb:Luna_1
Venus missions
|
|
gptkbp:is_involved_in
|
gptkb:Monarch
|
|
gptkbp:is_used_for
|
gptkb:spacecraft
|
|
gptkbp:launch_date
|
gptkb:1966
|
|
gptkbp:launch_site
|
gptkb:Vostok_2
gptkb:Baikonur_Cosmodrome
ground launch
|
|
gptkbp:launch_vehicle
|
gptkb:Proton_rocket
gptkb:Venera_program
heavy-lift
|
|
gptkbp:launched
|
gptkb:Sputnik_1
gptkb:40
|
|
gptkbp:legacy
|
foundation for future rockets
|
|
gptkbp:length
|
34.0 m
|
|
gptkbp:manufacturer
|
gptkb:OKB-1
|
|
gptkbp:mass
|
280,000 kg
|
|
gptkbp:military_technology
|
ICBM development
|
|
gptkbp:mission
|
gptkb:Luna_program
gptkb:Vostok_1
|
|
gptkbp:notable_achievement
|
gptkb:first_human_in_space
|
|
gptkbp:notable_album
|
gptkb:Sputnik_1
|
|
gptkbp:notable_feature
|
two-stage design
|
|
gptkbp:number_of_stages
|
gptkb:RD-107
gptkb:RD-108
2
|
|
gptkbp:operated_by
|
gptkb:Soviet_space_program
|
|
gptkbp:operational_area
|
1957-1960s
|
|
gptkbp:project
|
gptkb:Mars_program
|
|
gptkbp:propulsion
|
gptkb:RP-1/_LOX
|
|
gptkbp:retired
|
1960s
|
|
gptkbp:seating_capacity
|
gptkb:battle
1,100 kg
|
|
gptkbp:successor
|
gptkb:R-7_A
gptkb:R-7_Semyorka
gptkb:Soyuz_program
|
|
gptkbp:used_in
|
gptkb:spacecraft
|
|
gptkbp:bfsParent
|
gptkb:R-7_A
|
|
gptkbp:bfsLayer
|
5
|