AMAT
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Contents:

  • About AMAT
  • Installation
  • Capabilities
  • Example Jupyter Notebooks
  • JSR Article Notebooks
  • Acta Astronautica Notebooks
    • Uranus Orbiter and Probe
      • Section 01 - Literature Survey
      • Section 02 - Mission Requirements
      • Section 03 - Tradespace Exploration
      • Section 04 - Approach Trajectory and Entry State
      • Section 05 - Aerocapture Entry Corridor and Limiting Trajectories
      • Section 06 - Effect of Atmospheric Uncertainties
      • Section 07 - Guidance Scheme
      • Section 08 - Performance Analysis
      • Section 08 - Performance Analysis - A - 3X Higher EFPA uncertainty
      • Section 08 - Performance Analysis - B - 3X Lower EFPA uncertainty
      • Section 08 - Performance Analysis - C - 5X Higher atm uncertainty
      • Section 08 - Performance Analysis - D - 5X Lower atm uncertainty
      • Section 08 - Performance Analysis - E - lower lift-to-drag ratio
      • Section 08 - Performance Analysis - F - higher lift-to-drag ratio
      • Section 08 - Performance Analysis - G - stress case
      • Section 09 - Probe Delivery
      • Section 10 - Flight System Summary
  • MDPI Aerospace Notebooks
  • Other Notebooks
  • API Reference
  • Contributions
  • Credits
  • References
  • Module Index
AMAT
  • Acta Astronautica Notebooks
  • Edit on GitHub

Acta Astronautica Notebooks

Uranus Orbiter and Probe

Jupyter Notebooks associated with Girija (2022), A Flagship-class Uranus Orbiter and Probe Mission Concept using Aerocapture, Acta Astronautica, Vol. 202, pp. 104-118. DOI: 10.1016/j.actaastro.2022.10.005

  • Section 01 - Literature Survey
  • Section 02 - Mission Requirements
  • Section 03 - Tradespace Exploration
  • Section 04 - Approach Trajectory and Entry State
  • Section 05 - Aerocapture Entry Corridor and Limiting Trajectories
  • Section 06 - Effect of Atmospheric Uncertainties
  • Section 07 - Guidance Scheme
  • Section 08 - Performance Analysis
  • Section 08 - Performance Analysis - A - 3X Higher EFPA uncertainty
  • Section 08 - Performance Analysis - B - 3X Lower EFPA uncertainty
  • Section 08 - Performance Analysis - C - 5X Higher atm uncertainty
  • Section 08 - Performance Analysis - D - 5X Lower atm uncertainty
  • Section 08 - Performance Analysis - E - lower lift-to-drag ratio
  • Section 08 - Performance Analysis - F - higher lift-to-drag ratio
  • Section 08 - Performance Analysis - G - stress case
  • Section 09 - Probe Delivery
  • Section 10 - Flight System Summary
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© Copyright 2022, A.P. Girija. Revision 35590120.

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