Delta Cryogenic Second Stage (DCSS)
GPTKB entity
Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alternativeName |
gptkb:ICPS_(Interim_Cryogenic_Propulsion_Stage)
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
4.0 m
|
| gptkbp:engine |
gptkb:Pratt_&_Whitney_RL10B-2
|
| gptkbp:firstFlight |
1998
|
| gptkbp:height |
12.4 m
|
| https://www.w3.org/2000/01/rdf-schema#label |
Delta Cryogenic Second Stage (DCSS)
|
| gptkbp:manufacturer |
gptkb:Boeing
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
liquid hydrogen
|
| gptkbp:status |
active
|
| gptkbp:thrust |
110 kN
|
| gptkbp:usedOn |
gptkb:Delta_IV
gptkb:Delta_III gptkb:Orion_Artemis_I_(as_ICPS) |
| gptkbp:bfsParent |
gptkb:Interim_Cryogenic_Propulsion_Stage_(ICPS)
gptkb:Aerojet_Rocketdyne_RL10B-2 |
| gptkbp:bfsLayer |
7
|