Atmospheric entry
Label
Atmospheric entry
Name
Atmospheric entry
Source
nasat
Focus
Actions
Incoming Resources
- Subject of17
- Mars entry atmospheric data system modeling, calibration, and error analysis, Christopher D. Karlgaard [and four others]
- Optimizing facility configurations and operating conditions for improved performance in the NASA Ames EAST 24 inch shock tube, David W. Bogdanoff and Brett A. Cruden
- Entry, descent, and landing with propulsive deceleration, supersonic retropropulsion wind tunnel testing and shock phenomena, Bryan Palaszewski
- Phenolic Impregnated Carbon Ablators (PICA) as thermal protection systems for discovery missions, Huy K. Tran [and nine others]
- Flight data entry, descent, and landing (EDL) repository, Elmain M. Martinez and Daniel Winterhalter
- A multidisciplinary tool for systems analysis of planetary entry, descent, and landing (SAPE), Jamshid A. Samareh
- Parametric structural model for a Mars entry concept, Brittney M. Lane and Samee W. Ahmed
- Entry, descent and landing systems analysis study, phase 2 report on Mars Science Laboratory improvement, Mark C. Ivanov ... [and others]
- Multi-mission system analysis for planetary entry (M-SAPE) version 1, Jamshid Samareh [and thirteen others]
- Methods to determine the deformation of the IRVE Hypersonic Inflatable Aerodynamic Decelerator, William R. Young
- Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas, Parviz A. Bahrami
- Finite element modeling and analysis of Mars entry aeroshell concept, Samee W. Ahmed, Brittney M. Lane
- Aero-structural assessment of an inflatable aerodynamic decelerator, Essam F. Sheta ... [and others]
- Mars Phoenix EDL trajectory and atmosphere reconstruction using NewSTEP, Christopher D. Karlgaard and Jake A. Tynis
- Experimental investigation of Mars Science Laboratory entry vehicle aeroheating in AEDC hypervelocity tunnel 9, Brian R. Hollis, Arnold S. Collier
- Subsonic dynamics of stardust sample return capsule, R.A. Mitcheltree and C.M. Fremaux
- Uniform foam crush testing for multi-mission earth entry vehicle impact attenuation, Byron W. Patterson and Louis J. Glaab
Outgoing Resources
- Focus1