|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:constructionStartYear
|
1990s
|
|
gptkbp:cost
|
estimated $100 million (A5 variant)
|
|
gptkbp:countryOfOrigin
|
gptkb:Russia
|
|
gptkbp:designer
|
modular design
|
|
gptkbp:engineType
|
gptkb:RD-0124A
gptkb:RD-191
|
|
gptkbp:family
|
gptkb:Angara_1.2
gptkb:Angara_A3
gptkb:Angara_A5
gptkb:Angara_A5V
|
|
gptkbp:firstFlight
|
2014-07-09
|
|
gptkbp:fundedBy
|
gptkb:Russian_Federal_Space_Agency_(Roscosmos)
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Angara
|
|
gptkbp:launchSite
|
gptkb:Plesetsk_Cosmodrome
gptkb:Vostochny_Cosmodrome
|
|
gptkbp:manufacturer
|
gptkb:Khrunichev_State_Research_and_Production_Space_Center
|
|
gptkbp:notableMission
|
Angara 1.2 maiden flight 2014
Angara A5 maiden flight 2014
|
|
gptkbp:numberOfStages
|
2
|
|
gptkbp:payloadToGTO
|
up to 5,400 kg (A5 variant)
|
|
gptkbp:payloadToLEO
|
up to 24,500 kg (A5 variant)
|
|
gptkbp:propulsion
|
kerosene
liquid oxygen
|
|
gptkbp:purpose
|
orbital launch
|
|
gptkbp:replacedBy
|
older Russian launch vehicles
|
|
gptkbp:status
|
active
|
|
gptkbp:successor
|
gptkb:Proton_rocket
|
|
gptkbp:usedFor
|
military payloads
civilian payloads
|
|
gptkbp:bfsParent
|
gptkb:Yenisei
gptkb:Russland
gptkb:Russian_space_program
|
|
gptkbp:bfsLayer
|
5
|