Atmospheric entry
Resource Information
The concept Atmospheric entry represents the subject, aboutness, idea or notion of resources found in Missouri University of Science & Technology Library.
The Resource
Atmospheric entry
Resource Information
The concept Atmospheric entry represents the subject, aboutness, idea or notion of resources found in Missouri University of Science & Technology Library.
- Label
- Atmospheric entry
- Source
- nasat
27 Items that share the Concept Atmospheric entry
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- Wake flow about the Mars Pathfinder entry vehicle
- A multidisciplinary tool for systems analysis of planetary entry, descent, and landing (SAPE)
- Aero-structural assessment of an inflatable aerodynamic decelerator
- Entry dispersion analysis for the Stardust comet sample return capsule
- Entry, descent and landing systems analysis study : phase 2 report on Mars Science Laboratory improvement
- Entry, descent, and landing with propulsive deceleration : supersonic retropropulsion wind tunnel testing and shock phenomena
- Equilibrium radiative heating tables for aerobraking in the Martian atmosphere
- Equilibrium radiative heating tables for earth entry
- Estimates of thermochemical relaxation lengths behind normal shock waves relevant to manned lunar and Mars return missions, the aeroassist flight experiment, and Mars entry
- Experimental investigation of Mars Science Laboratory entry vehicle aeroheating in AEDC hypervelocity tunnel 9
- Finite element modeling and analysis of Mars entry aeroshell concept
- Flight data entry, descent, and landing (EDL) repository
- Mars Phoenix EDL trajectory and atmosphere reconstruction using NewSTEP
- Mars entry atmospheric data system modeling, calibration, and error analysis
- Methods to determine the deformation of the IRVE Hypersonic Inflatable Aerodynamic Decelerator
- Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas
- Multi-mission system analysis for planetary entry (M-SAPE) version 1
- Optimal trajectories for the aeroassisted flight experiment
- Optimal trajectories for the aeroassisted flight experiment, Part 2 Equations of motion in an inertial system
- Optimal trajectories for the aeroassisted flight experiment, Part 3 Fomulation, results, and analysis
- Optimizing facility configurations and operating conditions for improved performance in the NASA Ames EAST 24 inch shock tube
- Parametric structural model for a Mars entry concept
- Phenolic Impregnated Carbon Ablators (PICA) as thermal protection systems for discovery missions
- Phenolic Impregnated Carbon Ablators (PICA) as thermal protection systems for discovery missions
- Subsonic dynamics of stardust sample return capsule
- Uniform foam crush testing for multi-mission earth entry vehicle impact attenuation
- Use of random Martian atmosphere to evaluate potential entry guidance schemes
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.mst.edu/resource/JsIXhRlPULA/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.mst.edu/resource/JsIXhRlPULA/">Atmospheric entry</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.mst.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.mst.edu/">Missouri University of Science & Technology Library</a></span></span></span></span></div>
