Statements (52)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:computer
|
| gptkbp:applies_to |
launch vehicles
reentry vehicles |
| gptkbp:composed_of |
insulating materials
|
| gptkbp:developed_by |
gptkb:NASA
orbital reentry |
| gptkbp:enhances |
aerodynamic performance
|
| gptkbp:ensures |
crew safety
|
| https://www.w3.org/2000/01/rdf-schema#label |
Thermal Protection System
|
| gptkbp:includes |
gptkb:beer
coatings ablative materials radiative materials |
| gptkbp:is |
a protective measure
subject to testing a safety feature a critical component a performance enhancer used in various missions engineered for durability a focus of research a barrier against extreme conditions a component of spacecraft architecture a design consideration a field of study a method for heat management a part of aerospace technology a requirement for space missions a solution for thermal challenges a subject of engineering innovation a system for thermal regulation a technology for atmospheric entry a technology for space exploration designed to withstand heat essential for atmospheric reentry integral to spacecraft design |
| gptkbp:is_analyzed_in |
thermal stress
|
| gptkbp:is_critical_for |
gptkb:mission_success
|
| gptkbp:is_designed_for |
high-temperature environments
|
| gptkbp:is_evaluated_by |
computational fluid dynamics
|
| gptkbp:is_integrated_with |
airframe
|
| gptkbp:is_monitored_by |
flight tests
|
| gptkbp:is_protected_by |
heat
|
| gptkbp:is_subject_to |
extreme temperatures
|
| gptkbp:is_tested_for |
aerospace engineering
|
| gptkbp:provides |
thermal stability
|
| gptkbp:reduces |
heat transfer
|
| gptkbp:requires |
thermal analysis
|
| gptkbp:used_in |
gptkb:spacecraft
|
| gptkbp:utilizes |
thermal insulation
|
| gptkbp:bfsParent |
gptkb:robot
|
| gptkbp:bfsLayer |
3
|