Entry Heat Shields

Entry Heat Shields is a thermal protection system designed to mitigate extreme aerodynamic heating during atmospheric entry, distinguished by its use of ablative materials that dissipate heat through controlled surface recession and chemical decomposition.

Publications

Citations

177

Authors

Institutions

Publications per year

2017–2026

Parents

Ablative Materials

Publications

Technologies for thermal protection systems applied on re-usable launcher

Burkhard Behrens, Mark Müller · Acta Astronautica · 2004 · 133 citations

Engineering, Aerospace Engineering, Systems Engineering +13

Research progress on thermal protection materials and structures of hypersonic vehicles

Yazheng Yang, Jialing Yang, Daining Fang · Applied Mathematics and Mechanics · 2008 · 127 citations

Engineering, Aerospace Engineering, Materials Science +16

Experimental analysis of heat transfer within the AP600 containment under postulated accident conditions

Mark Anderson, L.E. Herranz, Michael L. Corradini · Nuclear Engineering and Design · 1998 · 117 citations

Engineering, Mechanical Engineering, Heat Transfer +16

Optimum design of ablative thermal protection systems for atmospheric entry vehicles

Aniello Riccio, Francesco Di Raimondo, Andrea Sellitto et al. · Applied Thermal Engineering · 2017 · 89 citations

Engineering, Aerospace Engineering, Systems Engineering +16

Reconstruction of Aerothermal Environment and Heat Shield Response of Mars Science Laboratory

Deepak Bose, Todd R. White, Milad Mahzari et al. · Journal of Spacecraft and Rockets · 2014 · 75 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

1–5 of 61

Authors

177

LY
Lily Yang
Ames Research Center, United States
5 publications · 83 citations
5
h-index
MM
Milad Mahzari
Ames Research Center, United States
5 publications · 150 citations
5
h-index
TR
Todd R. White
Ames Research Center, United States
5 publications · 150 citations
5
h-index
ME
Michael E. Tauber
Ames Research Center, United States
4 publications · 71 citations
4
h-index
WC
William C. Pitts
Stanford University, United States
3 publications · 104 citations
3
h-index

1–5 of 177

Institutions

1–8 of 52

Venues

Journal of Spacecraft and Rockets
10 publications · 256 citations
10
h-index
Fusion Engineering and Design
6 publications · 102 citations
6
h-index
AIAA Journal
3 publications · 124 citations
3
h-index
Journal of Thermophysics and Heat Transfer
3 publications · 82 citations
3
h-index
3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference
Conference · 2 publications · 38 citations
2
h-index

1–5