At the end of a rocket launch of a space vehicle from a launch site on the earth’s equator, the following burnout conditions hold. the burnout altitude is 110 km, and the burnout velocity vector lies in the equatorial plane with magnitude 8.3 km/s and flight path angle of 3 degrees above the local horizontal.
after burnout, the space vehicle moves along a two-body orbit.
(a) what is the specific angular momentum of the orbit of the space vehicle? what is the specific total energy of the orbit of the space vehicle?
(b) what is the orbital eccentricity?
an ldr's resistance changes with light intensity, while a thermistor's resistancce changes with temperature.
in dark, ldr's resistance is large and in the day/light ldr's resistance is small.
at low temperature, thermistor's resistance is large, while at large temperature it resistance is small.
in an ldr resistance increases as light intensity falls, while in a thermistor resistance falls as temperature falls.
the answer is
c. tilt of the axis
not too sure on this one maybe to locate objects under water, to diagnose problems, to treat medical ailments