|
gptkbp:instance_of
|
gptkb:stage_play
|
|
gptkbp:compatibility
|
ground support equipment
|
|
gptkbp:configuration
|
storable propellant
|
|
gptkbp:control_system
|
gptkb:navigation_system
|
|
gptkbp:debut
|
over 50 launches
|
|
gptkbp:design_purpose
|
to provide flexibility in launching missions
|
|
gptkbp:diameter
|
2.5 meters
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:environmental_concerns
|
designed for minimal impact
|
|
gptkbp:first_flight
|
gptkb:2000
gptkb:2021
|
|
gptkbp:guidance_system
|
autonomous
|
|
gptkbp:height
|
3.7 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fregat-MA
|
|
gptkbp:integration
|
short
|
|
gptkbp:launch_date
|
varies
|
|
gptkbp:launch_platform
|
centralized
|
|
gptkbp:launch_price
|
competitive
|
|
gptkbp:launch_site
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz
gptkb:Soyuz-2
|
|
gptkbp:manufacturer
|
gptkb:NPO_Lavochkin
|
|
gptkbp:mass
|
1,200 kg
|
|
gptkbp:mission
|
flexible
|
|
gptkbp:mission_duration
|
varies
|
|
gptkbp:mission_type
|
orbital insertion
|
|
gptkbp:notable_mission
|
gptkb:Gonets_satellites
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:operational_range
|
various orbits
|
|
gptkbp:operational_since
|
gptkb:2000
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:part_of
|
gptkb:Soyuz_family
|
|
gptkbp:payload_capacity
|
modular
adaptable
up to 3,000 kg
up to 1,500 kg
|
|
gptkbp:production_status
|
operational
|
|
gptkbp:project
|
ongoing improvements
|
|
gptkbp:propulsion
|
16.3
UDMH and N2 O4
19.6 k N
|
|
gptkbp:reliability
|
proven
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:strategic_goals
|
few
|
|
gptkbp:success
|
multiple
|
|
gptkbp:success_rate
|
high
|
|
gptkbp:used_for
|
launching satellites
|
|
gptkbp:user_countries
|
yes
multiple
|
|
gptkbp:bfsParent
|
gptkb:Kirov-class_cruisers
|
|
gptkbp:bfsLayer
|
6
|