|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:RD_family_of_engines
|
|
gptkbp:controls
|
inertial navigation
|
|
gptkbp:crew
|
gptkb:3
|
|
gptkbp:debut_year
|
1995-2000
|
|
gptkbp:decommissioned
|
gptkb:2000
|
|
gptkbp:design
|
modular
|
|
gptkbp:diameter
|
10.3 meters
|
|
gptkbp:engine
|
gptkb:4
|
|
gptkbp:engine_type
|
gptkb:RD-108
|
|
gptkbp:first_flight
|
1995-10-20
|
|
gptkbp:fuel_type
|
RP-1 and Liquid Oxygen
|
|
gptkbp:guidance_system
|
digital computer
|
|
gptkbp:height
|
46.3 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Soyuz-95 rocket
|
|
gptkbp:is_used_for
|
gptkb:uncrewed_missions
crewed missions
|
|
gptkbp:launch_date
|
annual
|
|
gptkbp:launch_site
|
gptkb:Arianespace
gptkb:Baikonur_Cosmodrome
gptkb:railway_station
|
|
gptkbp:launch_vehicle
|
gptkb:Soyuz
Site 1/5
295,000 kg
|
|
gptkbp:manufacturer
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:market
|
$30 million
|
|
gptkbp:mission
|
International Space Station resupply
suborbital and orbital
|
|
gptkbp:number_of_stages
|
gptkb:3
|
|
gptkbp:operational_area
|
1995-2000
|
|
gptkbp:orbital_inclination
|
51.6 degrees
|
|
gptkbp:propulsion
|
1,120 k N
|
|
gptkbp:replaced_by
|
gptkb:Soyuz-2
|
|
gptkbp:restoration
|
gptkb:musician
|
|
gptkbp:seating_capacity
|
2.5 meters
horizontal
7,000 kg
|
|
gptkbp:status
|
retired
|
|
gptkbp:strategic_importance
|
gptkb:0
|
|
gptkbp:succeeded_by
|
gptkb:10
100%
|
|
gptkbp:suspension
|
vertical
|