Apollo Lunar Module descent engine system
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:abbreviation |
gptkb:DPS
|
| gptkbp:alsoKnownAs |
gptkb:Descent_Propulsion_System
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:engineType |
pressure-fed
|
| gptkbp:firstFlight |
1969
|
| gptkbp:manufacturer |
gptkb:Space_Technology_Laboratories
|
| gptkbp:propulsion |
gptkb:Aerozine_50
gptkb:dinitrogen_tetroxide |
| gptkbp:throttleable |
yes
|
| gptkbp:thrust |
10,125 lbf
|
| gptkbp:usedFor |
gptkb:satellite
lunar descent lunar module ascent abort |
| gptkbp:usedIn |
gptkb:Apollo_11
gptkb:satellite gptkb:Apollo_12 gptkb:Apollo_16 gptkb:Apollo_17 gptkb:Apollo_14 gptkb:Apollo_15 |
| gptkbp:bfsParent |
gptkb:Apollo_Lunar_Module_radar
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Apollo Lunar Module descent engine system
|