Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
launch escape system
|
| gptkbp:consistsOf |
abort motor
attitude control motor jettison motor |
| gptkbp:developedBy |
gptkb:NASA
|
| gptkbp:firstFlight |
gptkb:Pad_Abort_1
|
| gptkbp:firstTestFlightDate |
2010-05-06
|
| https://www.w3.org/2000/01/rdf-schema#label |
Orion Launch Abort System
|
| gptkbp:length |
5.2 meters
|
| gptkbp:location |
gptkb:Kennedy_Space_Center
|
| gptkbp:mountedOn |
gptkb:Orion_crew_module
|
| gptkbp:partOf |
gptkb:Orion_spacecraft
|
| gptkbp:purpose |
crew safety
emergency escape |
| gptkbp:separatesAt |
main engine cutoff
|
| gptkbp:status |
operational
|
| gptkbp:testFlights |
gptkb:Ascent_Abort-2
2019-07-02 |
| gptkbp:usedFor |
gptkb:Artemis_missions
|
| gptkbp:usedOn |
gptkb:Space_Launch_System
|
| gptkbp:weight |
7,000 kg
|
| gptkbp:bfsParent |
gptkb:Orion_Launch_Abort_System_testing
gptkb:NASA_Langley_Research_Center gptkb:Apollo_Launch_Escape_System |
| gptkbp:bfsLayer |
6
|