This figure shows the entry vehicle deceleration in g's along its flight
path during the entry phase of the mission. As the probe enters at 7.5 km/second,
the deceleration forces produced by the atmosphere range from less than
10 micro g at time 0 (160 km) to about 20 g at 100 seconds (25 km). The
deceleration pulse produced by parachute deployment is clearly seen at 185
seconds (10 km).
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This figure shows entry vehicle deceleration in g along its flight path
during the entry phase of the mission. Deceleration is plotted in logarithmic
coordinates to reveal accelerations in the range 0.00001 to 20 g. These
measurements allow the atmospheric density, pressure and temperature profiles
to be calculated.
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