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Heat: The considerable kinetic and potential energy possessed by an orbiting spacecraft must be lost during re-entry. As the atmosphere decelerates the spacecraft, the energy is converted into a great deal of heat. This heat must be tolerated and/or minimised. The heat can be tolerated by using heat shields that use ablating surfaces (as used on Apollo capsules) or insulating surfaces (as used on the space shuttle). The heat can be minimised by taking longer to re-enter, thereby lengthening the time over which the energy is converted to heat. The space shuttle uses this technique. <?xml:namespace prefix = o ns = "urn:schemas-microsoft-comfficeffice" /><o></o>
g forces: The deceleration of a re-entering spacecraft also produces g forces, typically greater than those experienced during launch. High g forces can be better tolerated by reclining the astronaut, so that blood is not forced away from the brain, and by fully supporting the body. The g forces can be minimised by extending the re-entry, slowing the rate of descent. This strategy is employed by the space shuttle.
ok my uestion:
The Hertz experiment was thought, in 1888, to have provided the final experimental evidence of the nature of light. Discuss the methods employed by Hertz in the experiment and the model of light that his experimental results clearly supported 7marks
g forces: The deceleration of a re-entering spacecraft also produces g forces, typically greater than those experienced during launch. High g forces can be better tolerated by reclining the astronaut, so that blood is not forced away from the brain, and by fully supporting the body. The g forces can be minimised by extending the re-entry, slowing the rate of descent. This strategy is employed by the space shuttle.
ok my uestion:
The Hertz experiment was thought, in 1888, to have provided the final experimental evidence of the nature of light. Discuss the methods employed by Hertz in the experiment and the model of light that his experimental results clearly supported 7marks