|
gptkbp:instanceOf
|
upper stage rocket
|
|
gptkbp:application
|
satellite launch
|
|
gptkbp:chemicalFormula
|
N2O4
|
|
gptkbp:controls
|
inertial navigation system
|
|
gptkbp:diameter
|
2.5 meters
|
|
gptkbp:engine
|
1
|
|
gptkbp:engineConfiguration
|
Kuznetsov
|
|
gptkbp:engineType
|
liquid rocket engine
|
|
gptkbp:firstFlight
|
2000
2021
|
|
gptkbp:fuelType
|
hypergolic
|
|
gptkbp:future_plans
|
flexible mission profiles
|
|
gptkbp:gameFeatures
|
UDMH
|
|
gptkbp:height
|
3.7 meters
|
|
gptkbp:historicalEvent
|
evolved_from_Fregat
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fregat-M2M
|
|
gptkbp:inspiration
|
orbital insertion
|
|
gptkbp:internationalRelations
|
yes
|
|
gptkbp:is_used_in
|
gptkb:Soyuz_rocket
|
|
gptkbp:launchDate
|
varies annually
over 30 launches
|
|
gptkbp:launchSite
|
gptkb:Arianespace
Baikonur Cosmodrome
|
|
gptkbp:launchVehicle
|
gptkb:Soyuz_family
multiple launch vehicles
|
|
gptkbp:manufacturer
|
gptkb:Russian_Space_Forces
|
|
gptkbp:missions
|
multiple satellite deployments
|
|
gptkbp:offers
|
varies by mission
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:operationalHistory
|
2000
|
|
gptkbp:operationalRange
|
low_Earth_orbit_to_geostationary_transfer_orbit
|
|
gptkbp:passenger_traffic
|
1,500 kg
3,000 kg
adaptable fairing sizes
|
|
gptkbp:performances
|
multiple stages
|
|
gptkbp:propulsion
|
19.6 kN
|
|
gptkbp:provides
|
autonomous guidance
|
|
gptkbp:reliability
|
proven track record
|
|
gptkbp:succeededBy
|
high
over 90%
|
|
gptkbp:weight
|
1,200 kg
|