Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:application |
gptkb:fighter_aircraft
|
| gptkbp:combustor_type |
dual-spool turbojet
|
| gptkbp:designed_by |
gptkb:Moscow_Institute_of_Thermal_Technology
|
| gptkbp:diameter |
1.1 m
|
| gptkbp:engine |
mixed flow
|
| gptkbp:engine_configuration |
twin-shaft
|
| gptkbp:first_introduced |
gptkb:1983
|
| gptkbp:fuel_type |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-33 family
|
| gptkbp:length |
3.2 m
|
| gptkbp:notable_users |
gptkb:Algeria
gptkb:India gptkb:Russia gptkb:Serbia gptkb:Ukraine |
| gptkbp:propulsion |
80 k N
~270 |
| gptkbp:specific_impulse |
290 s
|
| gptkbp:used_in |
gptkb:Mikoyan_Mi_G-29
|
| gptkbp:variant |
RD-33, RD-33 MK, RD-33 M
|
| gptkbp:weight |
about 300 kg
|
| gptkbp:bfsParent |
gptkb:Klimov_RD-33_M
|
| gptkbp:bfsLayer |
7
|