|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:book
|
gptkb:RD-0210
|
|
gptkbp:commercialOperator
|
gptkb:International_Launch_Services
|
|
gptkbp:countryOfOrigin
|
gptkb:Russia
gptkb:Soviet_Union
|
|
gptkbp:diameter
|
7.4 m (with boosters)
|
|
gptkbp:firstFlight
|
1965-07-16
|
|
gptkbp:fuelType
|
unsymmetrical dimethylhydrazine (UDMH)
|
|
gptkbp:height
|
58.2 m (Proton-M)
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Proton rocket family
|
|
gptkbp:launchSite
|
gptkb:Baikonur_Cosmodrome
|
|
gptkbp:manufacturer
|
gptkb:Khrunichev_State_Research_and_Production_Space_Center
|
|
gptkbp:mass
|
705,000 kg (Proton-M)
|
|
gptkbp:notableMission
|
gptkb:Salyut_space_stations
gptkb:Mir_modules
gptkb:Zvezda_module_for_ISS
gptkb:Luna_missions
gptkb:ExoMars
gptkb:Venera_missions
Mars missions
|
|
gptkbp:notableVariant
|
gptkb:Proton-K
gptkb:Proton-M
|
|
gptkbp:numberOfLaunches
|
over 400
|
|
gptkbp:numberOfStages
|
gptkb:RD-253
3
4
|
|
gptkbp:oxidizer
|
nitrogen tetroxide
|
|
gptkbp:payload
|
gptkb:Elektro-L
gptkb:AsiaSat_satellites
gptkb:GLONASS_satellites
gptkb:Raduga_satellites
gptkb:Spektr-RG
gptkb:Ekspress-AMU1
gptkb:Eutelsat_satellites
gptkb:Express_satellites
gptkb:Inmarsat_satellites
gptkb:Yamal_satellites
|
|
gptkbp:payloadToGTO
|
up to 6,300 kg
|
|
gptkbp:payloadToLEO
|
up to 23,000 kg
|
|
gptkbp:propulsion
|
hypergolic
|
|
gptkbp:retired
|
2025
|
|
gptkbp:status
|
active
retiring
|
|
gptkbp:successor
|
gptkb:Angara_rocket_family
|
|
gptkbp:thirdStageEngines
|
gptkb:RD-0213
|
|
gptkbp:usedFor
|
launching satellites
launching space probes
launching modules for space stations
|
|
gptkbp:bfsParent
|
gptkb:Proton-K
gptkb:Proton-M/Briz-M
|
|
gptkbp:bfsLayer
|
6
|