|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:capacity
|
one cosmonaut
|
|
gptkbp:communication_system
|
gptkb:radio_station
|
|
gptkbp:control_system
|
manual and automatic
|
|
gptkbp:cooling_system
|
phenolic resin
|
|
gptkbp:country
|
gptkb:Soviet_Union
|
|
gptkbp:crew
|
gptkb:none
gptkb:Gherman_Titov
gptkb:Andriyan_Nikolayev
gptkb:Valentina_Tereshkova
gptkb:Yuri_Gagarin
gptkb:Pavel_Popovich
|
|
gptkbp:crew_capacity
|
gptkb:1
|
|
gptkbp:debut
|
gptkb:1955
gptkb:Vostok_6
gptkb:Vostok_1
|
|
gptkbp:designed_by
|
gptkb:OKB-1
|
|
gptkbp:diameter
|
2.5 m
|
|
gptkbp:first_female_in_space
|
gptkb:Valentina_Tereshkova
|
|
gptkbp:first_female_spaceflight
|
gptkb:Valentina_Tereshkova
|
|
gptkbp:first_flight
|
gptkb:Yuri_Gagarin
August 6, 1963
April 12, 1961
return safely to Earth
carry a human into space
complete an orbital flight
|
|
gptkbp:flight_style
|
gptkb:6
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Vostok spacecraft
|
|
gptkbp:influenced
|
gptkb:subsequent_Soviet_space_programs
international space exploration
subsequent Soviet missions
|
|
gptkbp:influenced_by
|
gptkb:Mercury_program
V-2 rocket technology
|
|
gptkbp:instruments
|
gptkb:scientific_experiments
|
|
gptkbp:landing_distance
|
gptkb:parachute
|
|
gptkbp:launch_date
|
August 6, 1963
April 12, 1961
|
|
gptkbp:launch_mass
|
4,725 kg
|
|
gptkbp:launch_platform
|
ground launch
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Vostok_8_K72_K
|
|
gptkbp:launched
|
gptkb:6
|
|
gptkbp:length
|
4.5 m
|
|
gptkbp:life_support_system
|
oxygen and CO2 scrubbers
|
|
gptkbp:manufacturer
|
gptkb:Soviet_space_program
|
|
gptkbp:mission
|
gptkb:5
gptkb:Moscow
gptkb:Vostok_6
|
|
gptkbp:mission_duration
|
up to 10 days
1 hour 48 minutes
|
|
gptkbp:mission_type
|
gptkb:human_spaceflight
|
|
gptkbp:notable_feature
|
gptkb:navigation_system
gptkb:health_services
gptkb:reentry_capsule
gptkb:launch_escape_system
gptkb:photography
thermal protection system
temperature control system
spherical shape
parachute recovery system
radio communication with ground control
emergency systems
orbital maneuvering system
stabilization fins
automatic stabilization system
crew cabin design
ejection seat for crew escape
recovery parachute system
reentry trajectory control
scientific instruments on board
single-use design
|
|
gptkbp:notable_mission
|
gptkb:Vostok_6
gptkb:Vostok_1
|
|
gptkbp:operational_period
|
1961 to 1963
|
|
gptkbp:orbital_altitude
|
200 to 300 km
|
|
gptkbp:orbital_inclination
|
65 degrees
|
|
gptkbp:orbital_period
|
about 90 minutes
|
|
gptkbp:power_source
|
gptkb:battery
silver-zinc batteries
|
|
gptkbp:recovery_method
|
parachute landing
water landing
|
|
gptkbp:significance
|
first crewed space program
|
|
gptkbp:spacecraft
|
gptkb:capsule
|
|
gptkbp:speed
|
28,000 km/h
ballistic
|
|
gptkbp:successor
|
gptkb:Voshkod_spacecraft
|
|
gptkbp:weight
|
4,725 kg
|
|
gptkbp:bfsParent
|
gptkb:Soyuz_spacecraft
gptkb:Vostok_program
gptkb:Vostok_1
gptkb:Soviet_space_program
|
|
gptkbp:bfsLayer
|
4
|