Aerothermodynamic and control system parameters and performance are discussed. Aerocapture trajectories were run for several combinations of entry path angles and velocities for the SO2P, MSR, and Uranus missions. The SO2P trajectories represent a Titan atmospheric entry for orbit about Saturn; the MSR trajectories represent a Mars atmospheric entry for orbit about Mars; similarly, the Uranus trajectories enter an Uranus atmosphere to achieve orbit about Uranus.


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    Titel :

    Generic Aerocapture Atmospheric Entry Study. Volume 2: Trajectory Appendices


    Erscheinungsdatum :

    1980


    Format / Umfang :

    159 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch