Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:rocket
|
| gptkbp:bfsLayer |
7
|
| gptkbp:bfsParent |
gptkb:Ne-20_turbojet_engine
|
| gptkbp:aircraft_operated |
gptkb:Mikoyan_Mi_G-31
|
| gptkbp:application |
gptkb:rocket
|
| gptkbp:average_temperature |
1,500 K
|
| gptkbp:check_in_time |
gptkb:battle
|
| gptkbp:compression_ratio |
8:1
|
| gptkbp:designed_by |
gptkb:Mikoyan
|
| gptkbp:developer |
gptkb:Monarch
|
| gptkbp:diameter |
1.1 m
|
| gptkbp:first_flight |
gptkb:1964
|
| gptkbp:fuel_type |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
AL-7 engine
|
| gptkbp:length |
4.2 m
|
| gptkbp:max_speed |
Mach 3.2
|
| gptkbp:number_of_rooms |
annular
|
| gptkbp:propulsion |
gptkb:12.5
15,000 lbf |
| gptkbp:replaced_by |
RD-36-35 engine
|
| gptkbp:service_ceiling |
20,000 m
|
| gptkbp:speed |
1,200 m/s
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:Mikoyan_Mi_G-25
|
| gptkbp:weight |
1,200 kg
|