[HTML][HTML] Advanced sandwich structures for thermal protection systems in hypersonic vehicles: A review
A heat shield called the thermal protection system (TPS) is an important structure in
hypersonic vehicles as it prevents hot air from entering vehicles and potential impacts from …
hypersonic vehicles as it prevents hot air from entering vehicles and potential impacts from …
[HTML][HTML] Multiscale, elastic, and low-density carbon fibre/siliconoxycarbide-phenolic interpenetrating aerogel nanocomposite for ablative thermal protection
X Jin, C Liu, H Huang, R Pan, C Wu, X Yan… - Composites Part B …, 2022 - Elsevier
Lightweight ablators are considered to be the most potential materials for ablative thermal
protection. Herein, a novel needle carbon fibre enhanced siliconoxycarbide-phenolic …
protection. Herein, a novel needle carbon fibre enhanced siliconoxycarbide-phenolic …
Performance of transpiration-cooled heat shields for reentry vehicles
T Hermann, M McGilvray, I Naved - AIAA Journal, 2020 - arc.aiaa.org
This paper presents results of a system study of transpiration-cooled thermal protection
systems for Earth reentry. The cooling performance for the sustained hypersonic flight and …
systems for Earth reentry. The cooling performance for the sustained hypersonic flight and …
[HTML][HTML] Quantification of feature variability in porous ablators
A crucial component of space vehicles is the thermal protection system (TPS), which protects
the vehicle from extreme heat loads. Morphological variations in TPS materials arising from …
the vehicle from extreme heat loads. Morphological variations in TPS materials arising from …
Design of new carbon-phenolic ablators: Manufacturing, plasma wind tunnel tests and finite element model rebuilding
L Paglia, V Genova, J Tirillò, C Bartuli… - Applied Composite …, 2021 - Springer
Ablative materials represent a widespread solution for shielding space vehicles from
overheating during a reentry phase in atmosphere where the high heating fluxes and the …
overheating during a reentry phase in atmosphere where the high heating fluxes and the …
Spallation of carbon ablators in arcjet facility experiments
F Grigat, S Löhle, M Eberhart, A Meindl… - … of Thermophysics and …, 2023 - arc.aiaa.org
Spallation is the mostly undesirable phenomenon where solid particles are ejected from
ablative materials leaving less mass to be decomposed at the ablator surface. The exact …
ablative materials leaving less mass to be decomposed at the ablator surface. The exact …
Measurement of the aerothermodynamic state in a high enthalpy plasma wind-tunnel flow
This paper presents spatially resolved measurements of absolute particle densities of N 2, N
2+, N, O, N+, O+, e− and excitation temperatures of electronic, rotational and vibrational …
2+, N, O, N+, O+, e− and excitation temperatures of electronic, rotational and vibrational …
An open carbon–phenolic ablator for scientific exploration
Abstract Space exploration missions rely on ablative heat shields for the thermal protection
of spacecraft during atmospheric entry flights. While dedicated research is needed for future …
of spacecraft during atmospheric entry flights. While dedicated research is needed for future …
Spallation on carbon ablators
A comprehensive analysis of publicly available research statements on spallation processes
of ablative heat shield materials is presented. Based on the published data and numerical …
of ablative heat shield materials is presented. Based on the published data and numerical …
Influence of ablation on vacuum-ultraviolet radiation in a plasma wind tunnel flow
Plasma wind tunnel experiments have been performed simulating a Hayabusa reentry
trajectory point at 78.8 km altitude with a velocity of 11.7 km/s corresponding to a local mass …
trajectory point at 78.8 km altitude with a velocity of 11.7 km/s corresponding to a local mass …