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limit aero-thermal heat flux
Definition
maximum or minimum local heat flux values, or the most unfavourable simultaneous combination of the constituting terms (in the sense of maximizing- or minimizing these heat fluxes) liable to be attained in the different areas of the vehicle during the normal service life for the corresponding mission instantNotes
- NOTE 1 Limit aero-thermal heat flux applies to TPS and hot structures only.
- NOTE 2 Aero-thermal fluxes can be caused by molecular flow and can also act after fairing jettisoning or at very low attitudes at orbital velocities.
Relations
- ECSS-E-ST-10-12C — flux
- ECSS-E-ST-10-12C — flux
- ECSS-E-ST-10-04C Rev.1 — flux
- ECSS-Q-ST-70-06C — flux
- ECSS-Q-ST-70-08C — flux
- ECSS-E-ST-31C — heat flux
- ECSS-E-ST-10-06C — mission
- ECSS-E-ST-70C — mission
- ECSS-S-ST-00-01C — mission
- ECSS-E-ST-50C — service
- ECSS-E-ST-70-41C — service
- ECSS-E-ST-40-07C — service
- ECSS-E-ST-32C Rev. 1 — service life
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