Jupiter probe heatshield configuration optimization

Details Jupiter probe heatshield configuration optimization Jupiter probe heatshield configuration optimization

May 1978

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978tpht.confq....d&link_type=abstract

American Institute of Aeronautics and Astronautics and American Society of Mechanical Engineers, Thermophysics and Heat Transfer

Physics

Ablative Nose Cones, Atmospheric Entry, Carbon-Carbon Composites, Heat Shielding, Jupiter Probes, Spacecraft Shielding, Blunt Bodies, Descent Trajectories, Jupiter Atmosphere, Optimization, Radiative Heat Transfer

Scientific paper

The effect of initial probe heatshield shape on the total probe mass loss during Jovian entry is considered. Modification of the aerothermal environment and probe entry trajectory due to changing probe heatshield shape is included in a computerized technique designed for rapid assessment of the effect of probe initial shape on heatshield mass loss. Results obtained indicate the importance of trajectory and heating distribution coupling with probe shape and mass change.

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