Apollo Lunar Module Descent Engine
GPTKB entity
Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:alsoKnownAs |
gptkb:LMDE
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:designer |
gptkb:TRW
|
| gptkbp:diameter |
1.5 m
|
| gptkbp:engineCycle |
pressure-fed
|
| gptkbp:firstFlight |
1969
|
| gptkbp:fuelType |
gptkb:Aerozine_50
|
| https://www.w3.org/2000/01/rdf-schema#label |
Apollo Lunar Module Descent Engine
|
| gptkbp:length |
1.65 m
|
| gptkbp:manufacturer |
gptkb:Space_Technology_Laboratories
|
| gptkbp:notableFeature |
first throttleable engine used for crewed lunar landing
|
| gptkbp:oxidizer |
gptkb:dinitrogen_tetroxide
|
| gptkbp:propulsion |
hypergolic
|
| gptkbp:status |
retired
|
| gptkbp:throttleRange |
10% to 100%
|
| gptkbp:thrust |
10,125 lbf
45 kN |
| gptkbp:usedFor |
gptkb:satellite
lunar descent |
| gptkbp:usedIn |
gptkb:Apollo_11
gptkb:satellite gptkb:Apollo_12 gptkb:Apollo_16 gptkb:Apollo_program gptkb:Apollo_17 gptkb:Apollo_14 gptkb:Apollo_15 |
| gptkbp:weight |
180 kg
|
| gptkbp:bfsParent |
gptkb:Mechanical_Engineering_Landmark_(ASME)
|
| gptkbp:bfsLayer |
5
|