Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:decommissioned |
1945
|
| gptkbp:developed_by |
gptkb:Germany
|
| gptkbp:engine_type |
liquid-fueled engine
|
| gptkbp:first_flight |
gptkb:1944
|
| gptkbp:guidance_system |
inertial guidance
|
| https://www.w3.org/2000/01/rdf-schema#label |
V-2 program
|
| gptkbp:influenced |
gptkb:space_exploration
|
| gptkbp:launch_platform |
mobile launch platform
|
| gptkbp:launch_site |
gptkb:Peenemünde
|
| gptkbp:notable_person |
gptkb:Wernher_von_Braun
|
| gptkbp:payload_capacity |
1,000 kg
|
| gptkbp:range |
320 km
|
| gptkbp:speed |
5,760 km/h
|
| gptkbp:success_rate |
approximately 50%
|
| gptkbp:successor |
gptkb:A-4_rocket
|
| gptkbp:type |
gptkb:missile
|
| gptkbp:used_in |
gptkb:World_War_II
|
| gptkbp:bfsParent |
gptkb:A4_rocket
|
| gptkbp:bfsLayer |
5
|