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gptkbp:instanceOf
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gptkb:spacecraft
|
|
gptkbp:communicationEquipment
|
S-band
|
|
gptkbp:controls
|
automatic control system
|
|
gptkbp:crew
|
gptkb:Mikhail_Tyurin
gptkb:Vladimir_Dezhurov
gptkb:Thomas_Reiter
simulator training
biomedical monitoring
|
|
gptkbp:crewCapacity
|
3
launch escape system
|
|
gptkbp:culturalImpact
|
featured in documentaries
|
|
gptkbp:diedIn
|
closed-loop system
|
|
gptkbp:environmentalImpact
|
ablative heat shield
|
|
gptkbp:finalScore
|
decommissioned
|
|
gptkbp:firstAwarded
|
probe and drogue
|
|
gptkbp:firstFlight
|
gptkb:Soyuz_TM-26
gptkb:Soyuz_TM-1
|
|
gptkbp:historicalSignificance
|
part_of_the_Soyuz_program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz 95
|
|
gptkbp:internationalCooperation
|
partnership_with_ESA
|
|
gptkbp:landingGear
|
gptkb:Kazakhstan
soft landing
|
|
gptkbp:launchDate
|
1997-07-12
|
|
gptkbp:launched
|
2 minutes
automated launch sequence
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
7,200 kg
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz-U
|
|
gptkbp:legacy
|
influenced future spacecraft designs
|
|
gptkbp:manufacturer
|
gptkb:RSC_Energia
|
|
gptkbp:mission
|
crewed
|
|
gptkbp:missions
|
gptkb:Moscow_Mission_Control_Center
5 days
successful
manual and automatic
|
|
gptkbp:navigationEquipment
|
inertial navigation system
|
|
gptkbp:operationalHistory
|
served multiple missions
|
|
gptkbp:orbitalInclination
|
51.6 degrees
orbital module
|
|
gptkbp:payloadCapacity
|
1,000 kg
|
|
gptkbp:postRetirementCareer
|
recovery team
|
|
gptkbp:powers
|
solar panels
|
|
gptkbp:respondsTo
|
2,500 kg
descent module
|
|
gptkbp:retirementYear
|
replacement by newer models
|
|
gptkbp:returnPolicy
|
ballistic reentry
|
|
gptkbp:safetyFeatures
|
redundant systems
|
|
gptkbp:scientificName
|
microgravity research
|
|
gptkbp:secondaryMission
|
debriefing sessions
|
|
gptkbp:services
|
service module
|
|
gptkbp:status
|
retired
|
|
gptkbp:technology
|
detailed engineering documents
|