|
gptkbp:instance_of
|
gptkb:Space_Launch_System
|
|
gptkbp:collaboration
|
possible
|
|
gptkbp:configuration
|
gptkb:Angara_1.2
gptkb:Angara_A5_P
gptkb:Angara_A5_V
gptkb:Angara_A5
|
|
gptkbp:country_of_origin
|
gptkb:Russia
|
|
gptkbp:design
|
modular
|
|
gptkbp:developed_by
|
gptkb:Russian_Federal_Space_Agency
|
|
gptkbp:development
|
gptkb:1995
gptkb:2014
|
|
gptkbp:engine_type
|
liquid-fueled
|
|
gptkbp:first_flight
|
gptkb:2014
2014-07-09
|
|
gptkbp:fuel_type
|
kerosene and liquid oxygen
|
|
gptkbp:future_plans
|
upgraded versions
|
|
gptkbp:guidance_system
|
inertial navigation
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Angara launch system
|
|
gptkbp:intended_use
|
gptkb:Space_Launch_System
interplanetary missions
|
|
gptkbp:launch_date
|
varies
|
|
gptkbp:launch_mass
|
450,000 kg
|
|
gptkbp:launch_platform
|
automated
|
|
gptkbp:launch_price
|
estimated $50 million
|
|
gptkbp:launch_site
|
gptkb:Vandenberg_Space_Force_Base
gptkb:Plesetsk_Cosmodrome
|
|
gptkbp:launch_window
|
flexible
|
|
gptkbp:manufacturer
|
gptkb:Khrunichev_State_Research_and_Production_Space_Center
|
|
gptkbp:mission
|
interplanetary missions
GTO missions
LEO missions
MEO missions
|
|
gptkbp:notable_launches
|
gptkb:Sirius_satellite
gptkb:Angosat-1
gptkb:KAZSAT-2
gptkb:Kondor_satellite
Express AM-7
|
|
gptkbp:number_of_stages
|
gptkb:3
2
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:payload_capacity
|
4.5 m
13 m
5,400 kg
24,500 kg
|
|
gptkbp:primary_user
|
gptkb:Russian_government
commercial customers
|
|
gptkbp:propulsion
|
1,000 k N
|
|
gptkbp:reliability
|
high
|
|
gptkbp:successor
|
gptkb:Proton_launch_vehicle
|
|
gptkbp:uses_rocket_engine
|
gptkb:RD-191
|
|
gptkbp:bfsParent
|
gptkb:RD-191
|
|
gptkbp:bfsLayer
|
6
|