The Development of a CO2 Test Capability in the NASA JSC ARCJet for Mars Reentry Simulation (original) (raw)

Arc Jet Testing in a Shear Environment for Mars Science Laboratory Thermal Protection System

Jarvis Songer

41st AIAA Thermophysics Conference, 2009

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Survey of European and major ISC facilities for supporting Mars and sample return mission aerothermodynamics and tests required for thermal protection system and dynamic stability

Philippe Reynier

International Journal of Aerospace Engineering, 2011

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Modeling of Shock Tunnel Aeroheating Data on the Mars Science Laboratory Aeroshell

Hans Hornung

Journal of Thermophysics and Heat Transfer, 2006

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Aerothermal Testing for Project Orion Crew Exploration Vehicle

Benjamin Kirk

41st AIAA Thermophysics Conference, 2009

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IRS Ground-Testing Facilities: Thermal Protection System Development, Code Validation and Flight Experiment Development

Georg Herdrich

24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2004

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Aerothermal environment definition for a reusable experimental re-entry vehicle wing

Giuseppe Rufolo

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Pre-X Experimental Re-Entry Lifting Body: Design of Flight Test Experiments for Critical Aerothermal Phenomena

Paolo Baiocco

2007

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Arcjet Testing of Micro-Meteoroid Impacted Thermal Protection Materials

Parul Agrawal

44th AIAA Thermophysics Conference, 2013

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Multidimensional Testing of Thermal Protection Materials in the Arcjet Test Facility

Thomas Squire

10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, 2010

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Aerothermal Environment Definition for a Reusable Experimental Re-entry Vehicle Wing Leading edge

Giuseppe Rufolo, Francesco Battista

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Preliminary Thermal Analysis of a Mars Sample Return Earth Entry Vehicle

Amundsen John

34th Thermophysics Conference, 2000

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Orbiter Return to Flight Entry Aeroheating

David Driver

9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, 2006

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Development of Thermal Protection Materials for Future Mars Entry, Descent and Landing Systems

Max Blosser

10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, 2010

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Shock Tube Experiments for Earth and Mars Entry Conditions

David Bogdanoff

2009

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EXPERT: The ESA experimental re-Entry test-bed: System overview

J. Gavira

16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 2009

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Effects of chemistry in Mars entry and Earth re-entry

Gennaro Zuppardi

2018

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High intensity 5 eV atomic oxygen source and Low Earth Orbit (LEO) simulation facility

Jon Cross

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Low Earth orbital atomic oxygen environmental simulation facility for space materials evaluation

Bruce Banks

1993

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Pushing the limits of re-entry technology: an overview of the Efesto-2 project and the advancements in inflatable heat shields

Giuseppe Guidotti

Materials research proceedings, 2023

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Advanced Models for Prediction of High Altitude Aero-Thermal Loads of a Space Re-entry Vehicle

Aldo Bonfiglioli

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Time-varying entry heating profile replication with a rotating arc jet test article

Jay Grinstead

AIAA Atmospheric Flight Mechanics Conference, 2014

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An Aerothermodynamic Study of a Typical Re-entry Capsule

Giuliano Ranuzzi

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Aero-Thermal Trade-Off Analysis of the Italian USV Re-Entry Flying Test Bed

Pierpaolo Matteis

14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006

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EFESTO-2: European Flexible Heat Shields Advanced TPS Design and Tests for Future In-Orbit Demonstration-2

Barbara Tiseo

Aerotecnica Missili & Spazio, 2024

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The EFESTO project: Flexible TPS Design and Testing for Advanced European Re-entry System Based on Inflatable Heat Schields

Giuseppe Guidotti

Le Centre pour la Communication Scientifique Directe - HAL - Université Paris Descartes, 2022

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Atmospheric Entry Experiments at IRS

Monika Auweter-kurtz

2002

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Shock Layer Radiation Measurements and Analysis for Mars Entry

David Bogdanoff

2009

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Development of an Innovative Validation Strategy of Gas-Surface Interaction Modelling for Re-Entry Applications — TN4210 - Development and validation of numerical models in TAU

Markus Fertig

2015

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Aerothermal Analysis of a Sample-Return Reentry Capsule

Valerio Carandente

Fluid Dynamics and Materials Processing

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FP7/Space Project “HYDRA” Hybrid Ablative Development for Re-Entry in Planetary Atmospheric Thermal Protection

S. FLOREZ FERNANDEZ

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A Fast Thermal 1D Model to Study Aerospace Material Response Behaviors in Uncontrolled Atmospheric Entries

Camilla Agabiti

Materials

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