|
gptkbp:instanceOf
|
rocket stage
|
|
gptkbp:application
|
satellite deployment
|
|
gptkbp:controls
|
inertial navigation system
|
|
gptkbp:design
|
orbital insertion
|
|
gptkbp:developer
|
confidential
|
|
gptkbp:diameter
|
2.5 meters
|
|
gptkbp:engine
|
1
|
|
gptkbp:engineType
|
gptkb:KRD-012
|
|
gptkbp:firstFlight
|
2000
|
|
gptkbp:fuelType
|
kerosene and liquid oxygen
|
|
gptkbp:gameFeatures
|
RP-1_and_Liquid_Oxygen
|
|
gptkbp:height
|
3.7 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fregat-MAE
|
|
gptkbp:launchDate
|
multiple successful launches
|
|
gptkbp:launched
|
gptkb:Arianespace
over 90%
varies annually
varies by mission
|
|
gptkbp:launchSite
|
Baikonur Cosmodrome
1,000 kg
|
|
gptkbp:launchVehicle
|
Soyuz,_Zenit
|
|
gptkbp:manufacturer
|
gptkb:Russia
Kosmotras
|
|
gptkbp:missionCapabilities
|
geostationary transfer orbit
|
|
gptkbp:notableFeature
|
multiple commercial satellites
|
|
gptkbp:number_of_stages
|
1
|
|
gptkbp:operationalArea
|
commercial and governmental missions
|
|
gptkbp:operationalStatus
|
2000
active
|
|
gptkbp:passenger_traffic
|
optional
|
|
gptkbp:payloadCapacity
|
1,500 kg to GTO
|
|
gptkbp:propulsion
|
30:1
30 kN
|
|
gptkbp:provides
|
autonomous guidance
|
|
gptkbp:reliability
|
very reliable
|
|
gptkbp:succeededBy
|
high
|
|
gptkbp:usedIn
|
Soyuz-2 launch vehicle
|
|
gptkbp:weight
|
1,000 kg
|