Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:spaceflight_maneuver
|
| gptkbp:abbreviation |
gptkb:TLI
|
| gptkbp:category |
gptkb:satellite
lunar missions orbital mechanics |
| gptkbp:describedBy |
NASA technical documents
spaceflight textbooks |
| gptkbp:first_used_by |
gptkb:Luna_1
|
| gptkbp:first_used_in_year |
1959
|
| gptkbp:involves |
firing a rocket engine
|
| gptkbp:purpose |
to send a spacecraft from Earth orbit toward the Moon
|
| gptkbp:relatedTo |
gptkb:Hohmann_transfer
gptkb:Trans-Mars_Injection |
| gptkbp:requires |
precise timing
calculated velocity change |
| gptkbp:result |
spacecraft entering a trajectory to intercept the Moon
|
| gptkbp:used_in_mission |
gptkb:Apollo_program
gptkb:Artemis_program |
| gptkbp:bfsParent |
gptkb:TLI
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Trans-Lunar Injection
|