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    An Analysis of Ablation-Shield Requirements for Manned Reentry Vehicles (1960)
    In:  CASI
    Details
    Publication Date: 2019-08-17
    Description: The problem of sublimation of material and accumulation of heat in an ablation shield is analyzed and the results are applied to the reentry of manned vehicles into the earth's atmosphere. The parameters which control the amount of sublimation and the temperature distribution within the ablation shield are determined and presented in a manner useful for engineering calculation. It is shown that the total mass loss from the shield during reentry and the insulation requirements may be given very simply in terms of the maximum deceleration of the vehicle or the total reentry time.
    Keywords: Spacecraft Design, Testing and Performance
    Type: NASA-TR-R-62
    Format: application/pdf
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