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Unformatted text preview: 3. Suppose the LANDSAT satellite of problem 1 d),e),f) (see Anderson 8.9) uses its thrusters, while at apogee, to increase its speed by 320m.s-1 . What will the new orbit semimajor axis and eccentricity? By how much will the next perigee altitude be increased?...
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This note was uploaded on 01/26/2012 for the course AE AE 202 taught by Professor Martin during the Spring '09 term at University of Illinois, Urbana Champaign.
- Spring '09