Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:Team_Rocket
|
| gptkbp:diameter |
5.1 meters
|
| gptkbp:engine_type |
gptkb:RL10
|
| gptkbp:first_flight |
gptkb:2002
|
| gptkbp:has_programs |
gptkb:Evolved_Expendable_Launch_Vehicle_(EELV)
|
| gptkbp:height |
4.1 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
Delta IV Upper Stage
|
| gptkbp:launch_site |
gptkb:Vandenberg_Space_Force_Base
gptkb:Cape_Canaveral_Space_Force_Station |
| gptkbp:launched |
gptkb:30
|
| gptkbp:manufacturer |
gptkb:United_Launch_Alliance
|
| gptkbp:mission |
low Earth orbit
geostationary transfer orbit |
| gptkbp:notable_mission |
gptkb:NASA's_Orion_spacecraft
gptkb:GPS_satellites National Reconnaissance Office payloads |
| gptkbp:number_of_engines |
gptkb:1
|
| gptkbp:operational_status |
retired
|
| gptkbp:payload_capacity |
4,000 kg
5,000 kg |
| gptkbp:propulsion |
liquid hydrogen and liquid oxygen
25,000 lbf |
| gptkbp:successor |
Centaur upper stage
|
| gptkbp:used_in |
gptkb:Delta_IV_rocket
|
| gptkbp:bfsParent |
gptkb:Interim_Cryogenic_Propulsion_Stage_(ICPS)
|
| gptkbp:bfsLayer |
6
|