Statements (53)
| Predicate | Object |
|---|---|
| gptkbp:can_be |
gptkb:Starship_upper_stage
|
| gptkbp:controls |
flight computer
|
| gptkbp:developed_by |
gptkb:2016
gptkb:Space_X |
| gptkbp:durability |
gptkb:theorem
|
| gptkbp:enables |
interplanetary travel
|
| gptkbp:fuel_type |
liquid methane and liquid oxygen
|
| gptkbp:height |
approximately 70 meters
|
| https://www.w3.org/2000/01/rdf-schema#label |
first stage
|
| gptkbp:is_designed_for |
high thrust
heavy lift capabilities |
| gptkbp:is_designed_to |
on a platform
orbital velocity |
| gptkbp:is_equipped_with |
grid fins
|
| gptkbp:is_expected_to |
reduce launch costs
improve launch reliability increase launch frequency support lunar missions enable deep space exploration enhance payload capacity enhance international collaboration in space facilitate space tourism contribute to space infrastructure development full reusability provide access to low Earth orbit reduce time to orbit support scientific research missions |
| gptkbp:is_integrated_with |
Starship vehicle
|
| gptkbp:is_monitored_by |
gptkb:railway_station
|
| gptkbp:is_part_of |
gptkb:Space_X's_Starship_program
gptkb:Super_Heavy gptkb:NASA_missions gptkb:starship commercial spaceflight initiatives global space economy Space X's future missions multi-stage launch system |
| gptkbp:is_subject_to |
regulatory approvals
|
| gptkbp:is_tested_for |
gptkb:Space_X
reliability static fire tests various payloads |
| gptkbp:is_used_for |
launching payloads
|
| gptkbp:launched |
gptkb:aircraft
|
| gptkbp:mass |
approximately 3,000,000 kg
|
| gptkbp:mission |
Mars colonization
|
| gptkbp:operated_by |
gptkb:Raptor_engines
|
| gptkbp:operates_in |
Earth's atmosphere
|
| gptkbp:released |
commercial payloads
|
| gptkbp:supports |
gptkb:spacecraft
satellite deployments |
| gptkbp:bfsParent |
gptkb:starship
|
| gptkbp:bfsLayer |
3
|