|
gptkbp:instance_of
|
gptkb:spacecraft
gptkb:rocket
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:State_Corporation_for_Activities_in_Space
|
|
gptkbp:aircraft_operated
|
3 days
|
|
gptkbp:communication
|
gptkb:radio_station
|
|
gptkbp:controls
|
gptkb:Soyuz_program
|
|
gptkbp:cooling_system
|
passive thermal control
|
|
gptkbp:crew
|
gptkb:Valery_Ryumin
gptkb:architect
gptkb:Alexander_Aleksandrov
gptkb:military_unit
gptkb:3
gptkb:Monarch
gptkb:Soyuz_descent_module
gptkb:Viktor_Savinykh
gptkb:Valery_Polyakov
gptkb:Alexander_Serebrov
all crew members healthy
first flight for Serebrov
second flight for Savinykh
third flight for Polyakov
|
|
gptkbp:date
|
1983-07-14
|
|
gptkbp:diameter
|
2.7 meters
|
|
gptkbp:duration
|
7 days
|
|
gptkbp:events
|
successful
|
|
gptkbp:first_flight
|
gptkb:musical
1983-04-05
|
|
gptkbp:has_programs
|
gptkb:Soyuz_program
|
|
gptkbp:height
|
7.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz-60
|
|
gptkbp:is_a_destination_for
|
gptkb:Salyut_7
|
|
gptkbp:is_aplace_for
|
200 kilometers
300 kilometers
|
|
gptkbp:landing_site
|
gptkb:1983
gptkb:Kazakhstan
1983-06-14
|
|
gptkbp:launch_date
|
gptkb:1983
1983-07-07
1983-06-07
10:00 UTC
06:00 UTC
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz-U
7,200 kg
|
|
gptkbp:manufacturer
|
gptkb:Soyuz_Design_Bureau
|
|
gptkbp:max_takeoff_weight
|
10:12 UTC
|
|
gptkbp:mission
|
gptkb:Scientific_research
gptkb:Soyuz-60_patch
gptkb:112
gptkb:Soyuz_60
gptkb:Research_Institute
126
success
successful
crewed
low Earth orbit
manned
crew transport
space station resupply
successful mission analysis.
|
|
gptkbp:mission_duration
|
7 days
168 hours
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operating_hours
|
7 days 22 hours 12 minutes
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operator
|
gptkb:Soviet_space_program
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:orbital_period
|
90 minutes
|
|
gptkbp:power_output
|
solar panels
|
|
gptkbp:predecessor
|
gptkb:Soyuz-59
|
|
gptkbp:propulsion
|
gptkb:Soyuz_T-10
gptkb:Soyuz_T-7
RP-1 and Liquid Oxygen
hypergolic propellants
|
|
gptkbp:scholarships
|
closed-loop system
|
|
gptkbp:seating_capacity
|
2.2 m
1,000 kg
7.2 m
3.4 m
|
|
gptkbp:services
|
gptkb:Soyuz_service_module
|
|
gptkbp:significant_event
|
first flight of Soyuz T-10 series
|
|
gptkbp:speed
|
28,000 km/h
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Soyuz-61
gptkb:Soyuz-T
|
|
gptkbp:team
|
Soviet recovery team
|
|
gptkbp:year_created
|
1983-07-14
|