Delta Cryogenic Second Stage
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:abbreviation |
gptkb:DCSS
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
4 meters
5 meters |
| gptkbp:engine |
gptkb:Aerojet_Rocketdyne_RL10B-2
|
| gptkbp:firstFlight |
1998
|
| gptkbp:fuelType |
liquid hydrogen
|
| https://www.w3.org/2000/01/rdf-schema#label |
Delta Cryogenic Second Stage
|
| gptkbp:length |
13.7 meters
|
| gptkbp:manufacturer |
gptkb:Boeing
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
cryogenic
|
| gptkbp:status |
active
|
| gptkbp:thrustVacuum |
110 kN
|
| gptkbp:usedOn |
gptkb:Delta_IV
gptkb:Delta_IV_Heavy gptkb:Delta_III gptkb:Space_Launch_System_Block_1 gptkb:Orion_Artemis_I |
| gptkbp:bfsParent |
gptkb:RL10_engine
gptkb:Interim_Cryogenic_Propulsion_Stage gptkb:RL10 |
| gptkbp:bfsLayer |
6
|