DCSS (Delta Cryogenic Second Stage)
GPTKB entity
Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alternativeName |
gptkb:ICPS_(Interim_Cryogenic_Propulsion_Stage)
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
4 meters
5 meters |
| gptkbp:engine |
gptkb:Pratt_&_Whitney_RL10B-2
|
| gptkbp:firstFlight |
1998
|
| https://www.w3.org/2000/01/rdf-schema#label |
DCSS (Delta Cryogenic Second Stage)
|
| gptkbp:manufacturer |
gptkb:Boeing
|
| gptkbp:propulsion |
liquid oxygen
liquid hydrogen |
| gptkbp:status |
active
|
| gptkbp:thrustVacuum |
110 kN
|
| gptkbp:usedOn |
gptkb:Delta_IV
gptkb:Delta_III gptkb:Orion_Artemis_I_(as_ICPS) |
| gptkbp:bfsParent |
gptkb:RL10_engine
|
| gptkbp:bfsLayer |
6
|