Reference mission 3B ascent trajectory. Mission planning, mission analysis and software formulation


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    • NASA  status
      (13.33%) (3 Votes)
      Views: (1514)   Date: (Feb 11, 1975)   Pages: ()
    • Author:  Kuhn  A. E.  

    • Abstract:  Mission 3B is designed as a payload retrieval mission with both shuttle launch and orbiter landing to take place at the western test range. The mission is designed for direct rendezvous with a passive satellite in a 100 NMI circular orbit with an inclination of 104 degrees. The ascent portion of mission 3B is described as well as the trajectory simulation.

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