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gptkbp:instance_of
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gptkb:rocket
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:RD_family_of_engines
|
|
gptkbp:controls
|
digital
|
|
gptkbp:country
|
widely used
|
|
gptkbp:debut_year
|
over 100 launches
|
|
gptkbp:design
|
to place payloads into orbit
|
|
gptkbp:developer
|
ongoing
|
|
gptkbp:diameter
|
2.5 meters
|
|
gptkbp:elevation
|
up to 36,000 km
|
|
gptkbp:engine
|
gptkb:musical
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:fuel_type
|
gptkb:monomethylhydrazine
|
|
gptkbp:guidance_system
|
gptkb:hospital
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Briz upper stage
|
|
gptkbp:is_used_for
|
geostationary satellites
|
|
gptkbp:launch_date
|
varies annually
|
|
gptkbp:launch_site
|
gptkb:Guiana_Space_Centre
gptkb:Baikonur_Cosmodrome
gptkb:software
|
|
gptkbp:launch_vehicle
|
gptkb:Proton_rocket
gptkb:Proton-M
|
|
gptkbp:length
|
4.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Khrunichev_State_Research_and_Production_Space_Center
|
|
gptkbp:mass
|
1,200 kg
|
|
gptkbp:mission
|
gptkb:Yamal_300_K
gptkb:Eutelsat_3_B
gptkb:Intelsat_15
gptkb:SES-1
orbital insertion
Express AM-44
|
|
gptkbp:notable_features
|
modular design
advanced avionics
high reliability
high efficiency
reusable components
real-time telemetry
autonomous operation
flexible mission profiles
multiple payload deployment
long burn times
|
|
gptkbp:operational_area
|
gptkb:spacecraft
commercial satellites
government satellites
|
|
gptkbp:operational_status
|
gptkb:1994
active
|
|
gptkbp:propulsion
|
hydrazine
2,000 lbf
|
|
gptkbp:reliability
|
proven
|
|
gptkbp:seating_capacity
|
up to 5,000 kg to GTO
|
|
gptkbp:social_structure
|
gptkb:nitrogen_tetroxide
|
|
gptkbp:succeeded_by
|
high
|
|
gptkbp:successor
|
Briz-KM
|
|
gptkbp:tour
|
uses a single stage
|