Feasibility and Performance Analysis of Neptune Aerocapture Using Heritage Blunt-Body Aeroshells
2020
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...
- Correction
- Source
- Cite
- Save
- Machine Reading By IdeaReader
35
References
2
Citations
NaN
KQI