Ablative Heating Model is a computational framework within reentry trajectory analysis that characterizes thermal protection system performance by simulating material erosion and energy absorption through controlled ablation under extreme aerothermal conditions.
22
Publications
846
Citations
61
Authors
26
Institutions
Publications per year
2017–2026
2
Parents
Publications
22
Aerothermal environment for Jovian entry probes
James N. Moss, C. W. Bolz · 1976 · 60 citations
Engineering, Aerospace Engineering, Mechanical Engineering +17
Joseph Olejniczak, Michael Wright, Stuart J. Laurence et al. · 43rd AIAA Aerospace Sciences Meeting and Exhibit · 2005 · 55 citations
Engineering, Aerospace Engineering, Mechanical Engineering +15
1–5 of 22
Authors
61
- JO
2
h-index
- HG
2
h-index
- MW
2
h-index
- JB
1
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- SJ
1
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1–5 of 61
Institutions
26
Ames Research Center
Mountain View, United States
5 h-index
10 publications
462 citations
Langley Research Center
Hampton, United States
3 h-index
4 publications
112 citations
California Institute of Technology
Pasadena, United States
2 h-index
3 publications
142 citations
National Institute of Aerospace
Hampton, United States
1 h-index
1 publications
10 citations
Quantum Devices (United States)
Barneveld, United States
1 h-index
3 publications
42 citations
Science and Technology Corporation (United States)
Hampton, United States
1 h-index
1 publications
60 citations
Armagh Observatory & Planetarium
Armagh, United Kingdom
1 h-index
2 publications
70 citations
Academy of Medical Sciences
London, United Kingdom
1 h-index
3 publications
126 citations
1–8 of 26
Venues
- AIAA Journal
3 publications · 175 citations
3
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- 43rd AIAA Aerospace Sciences Meeting and Exhibit
2 publications · 87 citations
2
h-index
- 38th Aerospace Sciences Meeting and Exhibit
1 publications · 14 citations
1
h-index
- Acta Astronautica
1 publications · 42 citations
1
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- Lecture notes in computer science
LNCS · Book series · 1 publications · 69 citations
1
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1–5