Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
spaceflight maneuver
|
| gptkbp:abbreviation |
gptkb:TLI
|
| gptkbp:category |
space exploration
orbital mechanics |
| gptkbp:destination |
gptkb:Moon
|
| gptkbp:firstReleased |
1959
|
| https://www.w3.org/2000/01/rdf-schema#label |
Trans-lunar injection
|
| gptkbp:introducedIn |
gptkb:Luna_1_mission
|
| gptkbp:origin |
low Earth orbit
|
| gptkbp:performedBy |
upper stage of launch vehicle
|
| gptkbp:purpose |
to send a spacecraft from Earth orbit toward the Moon
|
| gptkbp:relatedTo |
gptkb:Hohmann_transfer
gptkb:Lunar_transfer_orbit gptkb:Trans-Mars_injection |
| gptkbp:requires |
precise timing
high velocity change |
| gptkbp:typicalDeltaV |
~3.2 km/s
|
| gptkbp:usedIn |
gptkb:Apollo_program
gptkb:Artemis_program gptkb:Lunar_Gateway_missions |
| gptkbp:bfsParent |
gptkb:S-IVB
|
| gptkbp:bfsLayer |
5
|