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| Instructors: |
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| Course Description: |
Orbital
trajectory design; analysis of vehicle sustained g-forces; vehicle vibration
analysis; orbital maneuvering; atmospheric re entery; lunch windows;
rocket apogee and down range computations; wind corrections and lunch
anagles. |
| Credit Hours: |
3 |
| Course Prerequisites: |
PHY
2053C, Calculus I, II, CAD. |
| Course Objectives:
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| Course links: |
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| Class Schedule: |
Tuesday and Thursday
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15:00-16:15
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ES1B KSC |
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