Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:culturalHeritage |
derived from Bell 8247
|
| gptkbp:diameter |
1.28 m
|
| gptkbp:engineType |
pressure-fed
|
| gptkbp:firstFlight |
1969
|
| gptkbp:fuelType |
gptkb:Aerozine_50
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lunar Module Ascent Engine
|
| gptkbp:lastFlight |
1972
|
| 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
3,500 lbf |
| gptkbp:usedFor |
lunar ascent
lunar orbit insertion |
| gptkbp:usedIn |
gptkb:Apollo_11
gptkb:Apollo_12 gptkb:Apollo_16 gptkb:Apollo_17 gptkb:Apollo_14 gptkb:Apollo_15 |
| gptkbp:usedOn |
gptkb:satellite
|
| gptkbp:weight |
180 kg
|
| gptkbp:bfsParent |
gptkb:Apollo_hardware
|
| gptkbp:bfsLayer |
7
|