Apollo Lunar Module ascent engine
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:diameter |
1.28 m
|
| gptkbp:firstFlight |
1969
|
| gptkbp:fuelType |
gptkb:Aerozine_50
|
| gptkbp:gimbalRange |
none
|
| https://www.w3.org/2000/01/rdf-schema#label |
Apollo Lunar Module ascent engine
|
| gptkbp:length |
1.65 m
|
| gptkbp:manufacturer |
gptkb:Bell_Aerosystems
|
| gptkbp:oxidizer |
gptkb:dinitrogen_tetroxide
|
| gptkbp:propulsion |
hypergolic
|
| gptkbp:restartable |
yes
|
| gptkbp:status |
retired
|
| gptkbp:thrust |
15.6 kN
|
| gptkbp:usedIn |
gptkb:Apollo_11
gptkb:satellite gptkb:Apollo_12 gptkb:Apollo_16 gptkb:Apollo_17 gptkb:Apollo_14 gptkb:Apollo_15 |
| gptkbp:weight |
180 kg
|
| gptkbp:bfsParent |
gptkb:Aerozine_50/N2O4
|
| gptkbp:bfsLayer |
5
|