Statements (74)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:TIE_fighter
|
| gptkbp:composed_of |
multiple segments
|
| gptkbp:constructed_in |
lightweight materials
low Earth orbit |
| gptkbp:contains |
radiators
|
| gptkbp:contributes_to |
station's overall mass
|
| gptkbp:designed_by |
gptkb:NASA
modular features |
| gptkbp:designed_for |
microgravity research
long-term space missions |
| gptkbp:enables |
robotic operations
|
| gptkbp:enhances |
station's capabilities
station's structural integrity |
| gptkbp:facilitates |
crew activities
|
| gptkbp:features |
multiple attachment points
|
| gptkbp:first_introduced |
gptkb:1998
|
| gptkbp:function |
structural support
|
| https://www.w3.org/2000/01/rdf-schema#label |
S13 Truss
|
| gptkbp:integrates_with |
other truss segments
|
| gptkbp:is_compatible_with |
various modules
|
| gptkbp:is_connected_to |
gptkb:S1_Truss
gptkb:Z1_Truss gptkb:S2_Truss gptkb:S3_Truss gptkb:S4_Truss gptkb:S5_Truss Node 1 PMA-2 |
| gptkbp:is_critical_for |
ISS operations
|
| gptkbp:is_designed_for |
safety and reliability
modular assembly |
| gptkbp:is_designed_to |
maximize space efficiency
withstand vibrations support various modules |
| gptkbp:is_evaluated_by |
performance metrics
scientific teams |
| gptkbp:is_implemented_in |
gptkb:Zarya_module
|
| gptkbp:is_integrated_with |
ISS framework
other ISS components |
| gptkbp:is_maintained_by |
NASA engineers
|
| gptkbp:is_monitored_by |
gptkb:ground
|
| gptkbp:is_part_of |
ISS assembly sequence
ISS infrastructure ISS assembly ISS assembly process ISS truss system |
| gptkbp:is_subject_to |
regular inspections
space environment |
| gptkbp:is_supported_by |
international partnerships
launch vehicles |
| gptkbp:is_tested_for |
structural integrity
simulated environments space debris impacts |
| gptkbp:is_used_for |
research purposes
power generation |
| gptkbp:is_used_in |
gptkb:space_exploration
|
| gptkbp:is_utilized_for |
gptkb:scientific_research
|
| gptkbp:is_utilized_in |
various missions
|
| gptkbp:length |
approximately 7.3 meters
|
| gptkbp:material |
aluminum
|
| gptkbp:operated_by |
gptkb:United_States
space shuttle missions international crew |
| gptkbp:part_of |
gptkb:Node_2
|
| gptkbp:provides |
power distribution
thermal control |
| gptkbp:supports |
solar arrays
science experiments external payloads |
| gptkbp:used_in |
gptkb:International_Space_Station
|
| gptkbp:utilizes |
advanced materials
|
| gptkbp:weight |
approximately 1,500 kilograms
|
| gptkbp:bfsParent |
gptkb:S1_Truss
|
| gptkbp:bfsLayer |
7
|