Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:rocket_booster
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:developedBy |
gptkb:Khrunichev_State_Research_and_Production_Space_Center
|
| gptkbp:diameter |
~2.9 meters
|
| gptkbp:engineType |
gptkb:RD-191
|
| gptkbp:feature |
deployable wing for flyback
reusable booster |
| gptkbp:intendedUse |
gptkb:Angara_rocket_family
|
| gptkbp:length |
~15 meters
|
| gptkbp:propulsion |
kerosene
liquid oxygen |
| gptkbp:recoveryMethod |
horizontal landing
|
| gptkbp:relatedTo |
gptkb:Angara_1.2
gptkb:Energia_launch_vehicle |
| gptkbp:status |
gptkb:prototype
not flown |
| gptkbp:unveiled |
2001
|
| gptkbp:bfsParent |
gptkb:RD-191_engine
gptkb:РД-191 |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Baikal booster
|