|
gptkbp:instance_of
|
gptkb:stage_play
|
|
gptkbp:application
|
Satellite launch
|
|
gptkbp:compatibility
|
Telemetry and tracking
|
|
gptkbp:control_system
|
Inertial navigation system
|
|
gptkbp:debut
|
Over 50 launches
|
|
gptkbp:design
|
15 years
|
|
gptkbp:diameter
|
2.5 meters
|
|
gptkbp:engine_type
|
Liquid rocket engine
|
|
gptkbp:first_flight
|
gptkb:2000
|
|
gptkbp:future_plans
|
Continued use
|
|
gptkbp:guidance_system
|
GPS and GLONASS
|
|
gptkbp:has_tour
|
Multiple stages
|
|
gptkbp:height
|
3.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fregat-M2 EM
|
|
gptkbp:key_feature
|
Versatile and reliable
|
|
gptkbp:launch_date
|
gptkb:Regular
|
|
gptkbp:launch_price
|
Variable
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
Soyuz, Proton
|
|
gptkbp:launched
|
Single or multiple payloads
|
|
gptkbp:manufacturer
|
gptkb:Russian_Space_Forces
|
|
gptkbp:mass
|
1,200 kg
|
|
gptkbp:mission
|
Orbit insertion
|
|
gptkbp:modifications
|
Fregat-MT, Fregat-SB
|
|
gptkbp:notable_launches
|
Multiple satellite deployments
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:operational_since
|
gptkb:2000
|
|
gptkbp:operational_status
|
Active
|
|
gptkbp:operational_use
|
gptkb:Space
|
|
gptkbp:payload_capacity
|
Adaptable
1,500 kg
3,000 kg
|
|
gptkbp:payload_capacity_sun_synchronous_orbit
|
1,200 kg
|
|
gptkbp:production_location
|
gptkb:Russia
|
|
gptkbp:production_status
|
In service
|
|
gptkbp:propulsion
|
16.67
UDMH and N2 O4
20 k N
|
|
gptkbp:reliability
|
Proven
|
|
gptkbp:safety_record
|
Good
|
|
gptkbp:specification
|
Advanced
|
|
gptkbp:success_rate
|
gptkb:High
|
|
gptkbp:used_in
|
gptkb:Soyuz-2_rocket
|
|
gptkbp:user_countries
|
gptkb:Yes
|
|
gptkbp:bfsParent
|
gptkb:Sovremenny-class_destroyer
gptkb:Sovremenny-class_destroyers
gptkb:Nikolai_Gerasimovich_Kuznetsov
|
|
gptkbp:bfsLayer
|
6
|