Russian Zarya module

GPTKB entity

Properties (56)
Predicate Object
gptkbp:instanceOf space module
gptkbp:CEO two solar arrays
gptkbp:communicationEquipment S-band and Ku-band
advanced communication system
gptkbp:communitySupport yes
gptkbp:controls Russian_control_system
gptkbp:crewCapacity 0
gptkbp:currentLocation gptkb:International_Space_Station
gptkbp:dataUsage yes
gptkbp:diedIn not applicable
gptkbp:dimensions 4.1 m diameter
gptkbp:electrification solar panels
gptkbp:environmentalImpact active thermal control system
gptkbp:firstAwarded gptkb:International_Space_Station
APAS
1998-12-1998
one forward and one aft
gptkbp:hasFunction storage and power
gptkbp:hasPartnershipsWith NASA
gptkbp:historicalResearch supports various experiments
gptkbp:historicalSignificance first component of ISS
https://www.w3.org/2000/01/rdf-schema#label Russian Zarya module
gptkbp:internationalCooperation yes
gptkbp:is_integrated_with integrated into ISS
gptkbp:launchDate 1998-12-20
part_of_ISS_assembly
gptkbp:launched successful launch
gptkbp:launchSite gptkb:Russian_Federal_Space_Agency
gptkb:Kennedy_Space_Center
19,300 kg
gptkbp:launchVehicle Space Shuttle
gptkbp:length 12.56 m
gptkbp:maintenance requires periodic maintenance
gptkbp:manufacturer gptkb:Boeing
gptkbp:mission operational
uncrewed spacecraft
cylindrical design
19,300 kg
long-term endurance in space
low_Earth_orbit
gptkbp:operationalStatus active
gptkbp:orbitalInclination 51.6 degrees
gptkbp:payloadCapacity various scientific payloads
up to 2,000 kg
gptkbp:powers solar power system
gptkbp:productionYears expected 15 years
gptkbp:purpose providing power and storage
gptkbp:reliability high
gptkbp:researchInterest supports microgravity research
gptkbp:safetyFeatures multiple safety systems
gptkbp:scientificName various instruments onboard
gptkbp:sensors various scientific sensors
gptkbp:services functional module
gptkbp:supplyChain multiple resupply missions
gptkbp:voiceActor reaction control system
gptkbp:weight 19,300 kg