Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:spaceflight_maneuver
|
| gptkbp:alsoKnownAs |
gptkb:TMI
|
| gptkbp:destination |
gptkb:Mars
|
| gptkbp:field |
gptkb:astrodynamics
astronautics |
| gptkbp:introducedIn |
gptkb:Mariner_4
1964 |
| gptkbp:involves |
rocket engine burn
|
| gptkbp:origin |
gptkb:Earth_orbit
|
| gptkbp:performedBy |
gptkb:satellite
|
| gptkbp:purpose |
to send spacecraft from Earth orbit to Mars
|
| gptkbp:relatedTo |
gptkb:Trans-lunar_injection
gptkb:Hohmann_transfer_orbit |
| gptkbp:requires |
precise timing
high velocity change |
| gptkbp:usedIn |
interplanetary missions
|
| gptkbp:bfsParent |
gptkb:TMI
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Trans-Mars Injection
|