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Physics, 02.12.2019 19:10 lolorichards123

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?

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At the end of a rocket launch of a space vehicle from a launch site on the earth’s equator, the foll...
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