|
gptkbp:instance_of
|
gptkb:spacecraft
|
|
gptkbp:collaboration
|
limited
|
|
gptkbp:communication
|
gptkb:radio_station
|
|
gptkbp:communication_system
|
gptkb:radio_station
|
|
gptkbp:control_system
|
inertial navigation
|
|
gptkbp:cooling_system
|
ablative heat shield
|
|
gptkbp:crew
|
gptkb:Star_City
2
extensive
required
|
|
gptkbp:crew_capacity
|
gptkb:1
2
|
|
gptkbp:decommissioned
|
1970-12-31
|
|
gptkbp:design_features
|
modular design
|
|
gptkbp:designed_by
|
gptkb:Soviet_Union
|
|
gptkbp:development
|
1965-1967
|
|
gptkbp:diameter
|
2.2 m
|
|
gptkbp:duration
|
up to 10 days
|
|
gptkbp:first_flight
|
gptkb:1967
gptkb:1970
2
|
|
gptkbp:fuel_type
|
hypergolic propellant
|
|
gptkbp:height
|
3.2 m
|
|
gptkbp:historical_context
|
gptkb:Cold_War_space_race
|
|
gptkbp:historical_significance
|
first spacecraft designed for lunar missions
first crewed lunar mission attempt
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz 7 K-L1
|
|
gptkbp:inaugural_mission
|
gptkb:Zond_4
|
|
gptkbp:influenced
|
future spacecraft designs
|
|
gptkbp:influenced_by
|
gptkb:Apollo_program
|
|
gptkbp:inspiration
|
modern spacecraft designs
|
|
gptkbp:instruments
|
gptkb:sports_equipment
|
|
gptkbp:involved_in
|
gptkb:Moon
|
|
gptkbp:landing_distance
|
splashdown
|
|
gptkbp:landing_site
|
gptkb:Kazakhstan
|
|
gptkbp:launch_date
|
1967-03-01
1967-12-22
|
|
gptkbp:launch_mass
|
7,000 kg
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz_spacecraft
|
|
gptkbp:launch_window
|
limited
|
|
gptkbp:launched
|
gptkb:3
gptkb:5
December 22, 1966
|
|
gptkbp:legacy
|
paved the way for future missions
foundation for future Soyuz missions
|
|
gptkbp:length
|
7.2 m
|
|
gptkbp:life_support_system
|
closed-loop system
|
|
gptkbp:manufacturer
|
gptkb:OKB-1
|
|
gptkbp:mission
|
gptkb:Zond_8
gptkb:3
gptkb:Moscow
gptkb:Zond_7
partially successful
|
|
gptkbp:mission_duration
|
up to 10 days
|
|
gptkbp:mission_type
|
crewed
|
|
gptkbp:notable_features
|
reusable components
|
|
gptkbp:notable_mission
|
gptkb:Zond_4
|
|
gptkbp:number_built
|
gptkb:5
|
|
gptkbp:operated_by
|
gptkb:Soviet_space_program
|
|
gptkbp:operational_period
|
1967-1970
|
|
gptkbp:operational_status
|
retired
historical
|
|
gptkbp:orbital_altitude
|
200 km
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:power_source
|
solar panels
|
|
gptkbp:purpose
|
lunar missions
|
|
gptkbp:recovery_method
|
parachute landing
|
|
gptkbp:related_to
|
gptkb:Zond_program
|
|
gptkbp:related_vehicle
|
gptkb:Soyuz_descent_module
|
|
gptkbp:safety_record
|
high
mixed
|
|
gptkbp:specification
|
classified
|
|
gptkbp:speed
|
controlled
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Soyuz_7_K-OK
|
|
gptkbp:team
|
gptkb:Soviet_Navy
|
|
gptkbp:was
|
designed for lunar missions
|
|
gptkbp:weight
|
5,800 kg
5,000 kg
|
|
gptkbp:width
|
2.2 m
|
|
gptkbp:bfsParent
|
gptkb:Venera_13
gptkb:Venera_9
gptkb:Roscosmos
gptkb:Luna_16
|
|
gptkbp:bfsLayer
|
4
|