Properties (59)
Predicate | Object |
---|---|
gptkbp:instanceOf |
gptkb:spacecraft
|
gptkbp:aircraft |
three-module design
|
gptkbp:communicationEquipment |
VHF radio
|
gptkbp:crew |
gptkb:Star_City,_Russia
gptkb:Oleg_Makarov gptkb:Viktor_Patsayev Commander Research Engineer conducted during flight Valentin Lebedev via radio link Flight_Engineer |
gptkbp:crewCapacity |
gptkb:Soyuz_descent_module
|
gptkbp:crewSize |
3
based on experience |
gptkbp:duration |
168 hours
|
gptkbp:firstFlight |
1974-03-09
09:00 UTC conducted by engineers |
gptkbp:historicalSignificance |
part_of_the_Soviet_space_program
|
https://www.w3.org/2000/01/rdf-schema#label |
Soyuz 66
|
gptkbp:landingGear |
2,500 kg
Salyut 7 |
gptkbp:launchDate |
1974-03-02
10:00 UTC |
gptkbp:launched |
March 1974
T-10 minutes automated launch sequence Baikonur_launch_control |
gptkbp:launchSite |
Baikonur Cosmodrome
7,200 kg |
gptkbp:launchVehicle |
gptkb:Soyuz-U
|
gptkbp:manufacturer |
gptkb:OKB-1
|
gptkbp:mission |
gptkb:Soyuz_7K-OK
Low Earth Orbit crewed conducted before launch contributed to future missions |
gptkbp:missions |
gptkb:Moscow_Mission_Control
7 days completed successful extensive pre-flight training space station docking |
gptkbp:missionsConducted |
gptkb:Soyuz_66_patch
|
gptkbp:navigationEquipment |
inertial navigation
|
gptkbp:orbitalInclination |
51.6 degrees
perigee 200 km, apogee 300 km |
gptkbp:predecessor |
gptkb:Soyuz_65
|
gptkbp:renovated |
gptkb:Soviet_Air_Force
gptkb:Kazakhstan |
gptkbp:respondsTo |
standard reentry profile
|
gptkbp:safetyFeatures |
followed during mission
|
gptkbp:scientificName |
conducted in microgravity
|
gptkbp:secondaryMission |
conducted_by_Soviet_space_program
submitted_to_Soviet_authorities |
gptkbp:significance |
first crewed mission to Salyut 7
|
gptkbp:successor |
gptkb:Soyuz_67
|
gptkbp:technologyArea |
transmitted during mission
|