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.

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 Jet Propulsion Laboratory
surface form: 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 entry, descent, and landing modeling self-linksurface differs
surface form: Mars Science Laboratory mission
timePeriod post-landing reconstruction phase
pre-launch design and verification phase
usedBy Mars Science Laboratory entry, descent, and landing modeling self-linksurface differs
surface form: 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 entry, descent, and landing modeling self-linksurface differs
this entity surface form: Mars Science Laboratory mission
Mars Science Laboratory entry, descent, and landing modeling usedBy Mars Science Laboratory entry, descent, and landing modeling self-linksurface differs
this entity surface form: Mars Science Laboratory EDL team
sky crane maneuver partOf Mars Science Laboratory entry, descent, and landing modeling
this entity surface form: Entry Descent and Landing sequence