Answer: ha= 32 600 km 3/276 The Mars orbiter for the Viking mission was de-signed to make one complete trip around theplanet in exactly the same time that it takes Marsto revolve once about its own axis. This time is 24 h,37 min, 23 s. In this way, it is possible for the or-biter to pass over the landing site of the landercapsule at the same time in each Martian day atthe orbiter's minimum (periapsis) altitude. For theViking I mission, the periapsis altitude of the or-biter was 1508 km. Make use of the data in TableD/2 in Appendix D and compute the maximum(apoapsis) altitude ha for the orbiter in its ellipticalpath.hah,= 1508 kmProblem 3/276 PROBLEMS(Unless otherwise indicated, the velocities mentioned inthe problems which follow are measured from a nonrotat-ing reference frame moving with the center of the attract-ing body. Also, aerodynamic drag is to be neglected unlessstated otherwise. Use g = 9.825 m/s² (32.23 ft/sec²) for theabsolute gravitational acceleration at the surface of theearth and treat the earth as a sphere of radius R = 6371 km(3959 mi).)

Name: Answer: ha= 32 600 km 3/276 The Mars orbiter for the Viking mission wa
Uploaded: 2024-03-20T06:57:47.000Z
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Description: Answer: ha= 32 600 km 3/276 The Mars orbiter for the Viking mission was de-signed to make one complete trip around theplanet in exactly the same time that it takes Marsto revolve once about its own axis. This time is 24 h,37 min, 23 s. In this way, i