Mars Science Laboratory entry, descent, and landing modeling

E2741

Mars Science Laboratory entry, descent, and landing modeling is the suite of analytical and computational tools used to predict and optimize the Curiosity rover’s atmospheric entry, parachute descent, and landing performance on Mars.

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AI-generated illustration of Mars Science Laboratory entry, descent, and landing modeling

This AI-generated illustration was produced by black-forest-labs/FLUX.2-dev (1024x1024) from a prompt written by openai/gpt-oss-120b from the entity's label + description.

Prompt

Generate an image of Mars Science Laboratory entry, descent, and landing modeling (Mars Science Laboratory entry, descent, and landing modeling is the suite of analytical and computational tools used to predict and optimize the Curiosity rover’s atmospheric entry, parachute descent, and landing performance on Mars.)

All labels observed (4)

How this entity was disambiguated

Statements (48)

Predicate Object
instanceOf EDL simulation framework ⓘ
Mars mission engineering activity ⓘ
aerospace modeling suite ⓘ
computational analysis toolset ⓘ
appliesTo Curiosity rover ⓘ
constrains entry flight path angle ⓘ
heat shield thermal protection system design ⓘ
landing site safety margins ⓘ
parachute deployment Mach number ⓘ
peak deceleration loads ⓘ
developedBy NASA Jet Propulsion Laboratory ⓘ
developedFor Mars landing on 6 August 2012 ⓘ
focusesOn atmospheric entry performance ⓘ
parachute descent performance ⓘ
powered landing performance ⓘ
hasComponent descent modeling ⓘ
entry modeling ⓘ
landing modeling ⓘ
informed Curiosity EDL system design ⓘ
models Mars atmospheric density profiles ⓘ
aerodynamic forces and moments ⓘ
aerothermal heating loads ⓘ
back-shell separation dynamics ⓘ
landing impact conditions ⓘ
powered descent with retrorockets ⓘ
sky crane maneuver dynamics ⓘ
supersonic parachute performance ⓘ
partOf Mars Science Laboratory mission ⓘ
timePeriod post-landing reconstruction phase ⓘ
pre-launch design and verification phase ⓘ
usedBy Mars Science Laboratory EDL team ⓘ
usedFor Monte Carlo dispersion analysis ⓘ
aerothermal environment prediction ⓘ
design margin evaluation ⓘ
flight software verification ⓘ
landing ellipse determination ⓘ
parachute deployment analysis ⓘ
parachute inflation dynamics analysis ⓘ
risk assessment ⓘ
terminal descent guidance analysis ⓘ
trajectory prediction ⓘ
usesMethod 6-degree-of-freedom trajectory simulation ⓘ
Monte Carlo simulation ⓘ
aerothermal analysis ⓘ
computational fluid dynamics ⓘ
structural load analysis ⓘ
uncertainty quantification ⓘ
validatedBy Mars Science Laboratory flight data ⓘ

How these facts were elicited

Referenced by (4)

Full triples — surface form annotated when it differs from this entity's canonical label.

Ames Research Center → contributedTo → Mars Science Laboratory entry, descent, and landing modeling ⓘ
Mars Science Laboratory entry, descent, and landing modeling → partOf → Mars Science Laboratory mission ⓘ
linked to: Mars Science Laboratory entry, descent, and landing modeling
Mars Science Laboratory entry, descent, and landing modeling → usedBy → Mars Science Laboratory EDL team ⓘ
linked to: Mars Science Laboratory entry, descent, and landing modeling
sky crane maneuver → partOf → Entry Descent and Landing sequence ⓘ
linked to: Mars Science Laboratory entry, descent, and landing modeling