|
gptkbp:instance_of
|
gptkb:Team_Rocket
|
|
gptkbp:check_in_time
|
300 seconds
150 seconds
|
|
gptkbp:collaboration
|
yes
with other space agencies
|
|
gptkbp:configuration
|
A5
2-stage
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:country
|
gptkb:Russia
|
|
gptkbp:debut
|
TBD
planned for 2024
ongoing since 2014
first launch successful
|
|
gptkbp:design
|
gptkb:Khrunichev_State_Research_and_Production_Space_Center
|
|
gptkbp:design_purpose
|
replace Proton rocket
|
|
gptkbp:development
|
gptkb:Angara_rocket_family
gptkb:2000
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
3.8 meters
3.8 m
|
|
gptkbp:durability
|
no
not reusable
|
|
gptkbp:engine
|
RD-191 developed by NPO Energomash
|
|
gptkbp:engine_type
|
gptkb:RD-191
|
|
gptkbp:environmental_impact
|
assessed
assessed during development
|
|
gptkbp:first_flight
|
multiple
2020-12-27
2014-12-23
|
|
gptkbp:first_launch_success
|
gptkb:true
|
|
gptkbp:fuel_type
|
kerosene and liquid oxygen
|
|
gptkbp:future_plans
|
upgraded versions
|
|
gptkbp:guidance_system
|
gptkb:navigation_system
|
|
gptkbp:has_programs
|
gptkb:Russian_space_program
|
|
gptkbp:height
|
42 meters
47.8 m
65.3 meters
65.3 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Angara A5
|
|
gptkbp:integration
|
several months
|
|
gptkbp:intended_use
|
heavy-lift launch vehicle
|
|
gptkbp:launch_date
|
1-2 per year
approximately once a year
2014-12-23
|
|
gptkbp:launch_mass
|
450,000 kg
|
|
gptkbp:launch_platform
|
gptkb:Russian_Federal_Space_Agency
gptkb:Plesetsk_Launch_Control_Center
gptkb:Plesetsk_Cosmodrome
performed by Russian Space Agency
|
|
gptkbp:launch_price
|
estimated $50 million
estimated $100 million
|
|
gptkbp:launch_site
|
gptkb:Vandenberg_Space_Force_Base
gptkb:Plesetsk_Cosmodrome
|
|
gptkbp:launch_vehicle
|
gptkb:Angara
modular design
expendable
expendable launch vehicle
|
|
gptkbp:launch_window
|
varies by mission
|
|
gptkbp:launched
|
gptkb:3
gptkb:sports_equipment
military satellites
civilian satellites
|
|
gptkbp:manufacturer
|
gptkb:Khrunichev_State_Research_and_Production_Space_Center
|
|
gptkbp:media_coverage
|
extensive
extensive during launches
|
|
gptkbp:mission
|
gptkb:Russian_Space_Forces
gptkb:Russian_Mission_Control_Center
planned for various payloads
|
|
gptkbp:notable_launches
|
launch of military satellites
2020 military satellite
2021 scientific mission
2022 commercial payload
2023 government satellite
|
|
gptkbp:number_of_stages
|
gptkb:RD-0124
gptkb:3
2
four RD-191 engines
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:payload_capacity
|
4.5 m
13 m
4.0 m
5,400 kg
5 tons
24,500 kg
25 tons
13.0 m
24,500 kg to LEO
done at launch site
|
|
gptkbp:primary_mission
|
satellite deployment
|
|
gptkbp:propulsion
|
1,500 k N
1,600 k N
|
|
gptkbp:public_interest
|
high
high due to national pride
|
|
gptkbp:related_vehicle
|
gptkb:Angara_A3
gptkb:Angara_A1.2
gptkb:Angara_A6
|
|
gptkbp:release_country
|
not applicable
|
|
gptkbp:safety_record
|
good
no major incidents reported
|
|
gptkbp:specification
|
available online
available on official website
|
|
gptkbp:success_rate
|
100%
|
|
gptkbp:successor
|
gptkb:Angara_A5_P
|
|
gptkbp:supports
|
custom-built
|
|
gptkbp:transportation
|
rail and road
|
|
gptkbp:upgrades
|
planned upgrades for increased payload capacity
|
|
gptkbp:bfsParent
|
gptkb:Roscosmos
|
|
gptkbp:bfsLayer
|
4
|