Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:Descent_Propulsion_System
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:diameter |
59 inches
|
| gptkbp:firstFlight |
1969
|
| gptkbp:fuelType |
gptkb:Aerozine_50
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lunar Module Descent Engine
|
| gptkbp:length |
63 inches
|
| gptkbp:manufacturer |
gptkb:Space_Technology_Laboratories
|
| gptkbp:mission |
gptkb:Apollo_program
|
| gptkbp:oxidizer |
gptkb:dinitrogen_tetroxide
|
| gptkbp:propulsion |
hypergolic
|
| gptkbp:status |
retired
|
| gptkbp:throttleable |
true
|
| gptkbp:thrust |
10,125 lbf
1,050 to 10,125 lbf |
| gptkbp:usedBy |
gptkb:NASA
|
| gptkbp:usedIn |
gptkb:satellite
gptkb:Apollo_11_Lunar_Module_Eagle gptkb:Apollo_13_Lunar_Module_Aquarius |
| gptkbp:weight |
394 lb
|
| gptkbp:bfsParent |
gptkb:TRW
gptkb:TRW_Inc. |
| gptkbp:bfsLayer |
6
|