Orel spacecraft

GPTKB entity

Statements (54)
Predicate Object
gptkbp:instanceOf gptkb:spacecraft
gptkbp:airlines custom developed software
gptkbp:capacity 4 crew members
gptkbp:communicationEquipment S-band and Ku-band
gptkbp:controls fly-by-wire system
gptkbp:crew simulator training
biometric sensors
sleeping quarters and galley
gptkbp:crewCapacity emergency procedures
launch escape system
gptkbp:design modular design
gptkbp:designedBy gptkb:RSC_Energia
gptkbp:diameter 4.5 meters
gptkbp:diedIn up to 30 days
closed-loop system
gptkbp:emergencyServices land on solid ground
gptkbp:environmentalImpact ablative heat shield
temperature and humidity control
gptkbp:firstFlight 2023
planned for 2024
gptkbp:futurePlans Mars_missions
gptkbp:hasPartnershipsWith collaboration_with_NASA
gptkbp:historicalSignificance next generation of crewed spacecraft
https://www.w3.org/2000/01/rdf-schema#label Orel spacecraft
gptkbp:integration full system tests
gptkbp:internationalCooperation ESA_and_Roscosmos
gptkbp:landingGear parachute and airbag system
gptkbp:launched 2023-2024
extensive testing
annual missions
gptkbp:launchSite Baikonur Cosmodrome
gptkbp:launchVehicle gptkb:Soyuz-2.1b
gptkbp:length 9.2 meters
gptkbp:manufacturer gptkb:RSC_Energia
gptkbp:missionCapabilities low_Earth_orbit_missions
gptkbp:missions gptkb:MCC_Moscow
up to 30 days
gptkbp:navigationEquipment inertial navigation system
gptkbp:operationalStatus 200-400 km
gptkbp:orbitalInclination bi-propellant engine
gptkbp:passengerCapacity up to 500 kg
gptkbp:payloadCapacity pressurized and unpressurized
gptkbp:powers solar panels
gptkbp:productionCompany 2015
gptkbp:publicAccess high due to new technology
gptkbp:purpose crewed space missions
gptkbp:reliability partially reusable
gptkbp:renovated trained personnel
gptkbp:respondsTo separate return module
gptkbp:safetyFeatures redundant systems
gptkbp:scientificName various payloads
gptkbp:successor gptkb:Soyuz_spacecraft
gptkbp:sustainability focus on eco-friendly materials
gptkbp:weight 14,000 kg