Physics
Scientific paper
May 1978
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1978kosis..16..378g&link_type=abstract
Kosmicheskie Issledovaniia, vol. 16, May-June 1978, p. 378-387. In Russian.
Physics
4
Ablation, Aerodynamic Heating, Atmospheric Entry, Descent Trajectories, Jupiter Atmosphere, Jupiter Probes, Continuous Spectra, Equations Of Motion, Gas Dynamics, Hypersonic Heat Transfer, Iterative Solution, Line Spectra, Navier-Stokes Equation, Radiative Heat Transfer, Shock Waves, Trajectory Analysis
Scientific paper
The entry of probes into the Jovian atmosphere at speeds of 40 to 60 km/sec is analyzed with allowance for ablation. The equations of radiation gasdynamics are solved simultaneously with the equations of motion of the probe. Changes in the ballistic factor, due to ablation are taken into consideration. The thermal radiation fluxes are calculated with allowance for continuum and line radiative transfer. The influence of ablation on the descent path of a graphite-coated probe is determined.
Gershbein E. A.
Sukhodolskaia Ia. E.
Sukhodolskii S. L.
Tirskii G. A.
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