Statements (30)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:satellite
|
| gptkbp:contains |
fuel tanks
landing gear storage compartments descent engine |
| gptkbp:diameter |
about 4.2 meters (13.8 ft)
|
| gptkbp:function |
contain descent propulsion system
house scientific equipment provide landing platform |
| gptkbp:height |
about 3.2 meters (10.5 ft)
|
| https://www.w3.org/2000/01/rdf-schema#label |
Lunar Module Descent Stage
|
| gptkbp:manufacturer |
gptkb:Grumman_Aircraft_Engineering_Corporation
|
| gptkbp:mass |
approximately 10,334 kg (22,781 lb)
|
| gptkbp:nickname |
Descent Stage
|
| gptkbp:oxidizer |
N2O4 (nitrogen tetroxide)
|
| gptkbp:partOf |
gptkb:satellite
|
| gptkbp:propulsion |
gptkb:Aerozine_50
|
| gptkbp:remainsOn |
lunar surface
|
| gptkbp:thrust |
about 45 kN (10,000 lbf)
|
| gptkbp:usedFor |
gptkb:satellite
storing lunar surface experiments supporting ascent stage |
| gptkbp:usedIn |
gptkb:Apollo_11
gptkb:Apollo_12 gptkb:Apollo_16 gptkb:Apollo_17 gptkb:Apollo_14 gptkb:Apollo_15 |
| gptkbp:bfsParent |
gptkb:Lunar_Module_Ascent_Stage
|
| gptkbp:bfsLayer |
6
|