Feasibility and Performance Analysis of Neptune Aerocapture Using Heritage Blunt-Body Aeroshells,Journal of Spacecraft and Rockets

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Feasibility and Performance Analysis of Neptune Aerocapture Using Heritage Blunt-Body Aeroshells
Journal of Spacecraft and Rockets ( IF 1.3 ) Pub Date : 2020-11-01 , DOI: 10.2514/1.a34719
Athul Pradeepkumar Girija , Sarag J. Saikia , James M. Longuski , Shyam Bhaskaran , Matthew S. Smith , James A. Cutts

Large navigation and atmospheric uncertainties have historically driven the need for a mid-lift-to-drag-ratio (mid-L/D) vehicle with (L/D)max of 0.6–0.8 for aerocapture at Neptune. Most planetary e...

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