|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:countryOfOrigin
|
gptkb:Russia
|
|
gptkbp:derivedFrom
|
Phobos spacecraft propulsion module
|
|
gptkbp:diameter
|
3.35 m
|
|
gptkbp:engineType
|
gptkb:S5.92
|
|
gptkbp:firstFlight
|
2000-02-09
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Fregat upper stage
|
|
gptkbp:launchMass
|
6,700 kg
|
|
gptkbp:length
|
3.35 m
|
|
gptkbp:manufacturer
|
gptkb:NPO_Lavochkin
|
|
gptkbp:mass
|
930 kg
|
|
gptkbp:notableMission
|
gptkb:Galileo_satellites
gptkb:OneWeb_satellites
gptkb:Venus_Express
gptkb:Mars_Express
|
|
gptkbp:numberOfRestarts
|
up to 20
|
|
gptkbp:primaryUse
|
orbital insertion
payload deployment
|
|
gptkbp:propulsion
|
N2O4
UDMH
|
|
gptkbp:status
|
active
|
|
gptkbp:thrust
|
19.85 kN
|
|
gptkbp:totalProduced
|
yes
|
|
gptkbp:usedFor
|
gptkb:Soyuz_rocket
gptkb:Zenit_rocket
gptkb:Ariane_5_rocket
interplanetary missions
low Earth orbit missions
geostationary transfer orbit missions
medium Earth orbit missions
|
|
gptkbp:bfsParent
|
gptkb:NPO_Lavochkin
gptkb:Lavochkin
gptkb:Lavochkin_Association
gptkb:Lavochkin_design_bureau
gptkb:Fregat_M2EM
|
|
gptkbp:bfsLayer
|
6
|