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Request to add Proton Fluence report. #3

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10 changes: 10 additions & 0 deletions Reports/Radiation/Readme.md
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## Orbital Radiation Reports Directory
The following is a listing of reports found in this directory, along with their abstracts.

### Comparison of Orbital Proton Fluences For Proposed STP: Pearl Mission Orbits

This paper compares proton fluxes for four typical mission orbits: the MEO orbit; the Molniya HEO orbit; the TESS P/2 HEO orbit, and the Spitzer Earth Trailing
orbit (ETO); for more detail on individual orbits, see the STP Orbital Comparison memo. The proton
fluences are the result of SPENVIS modeling, with the exception of the ETO, which is cited from
Spitzer data. Illustrations of the orbital paths and their proximity to the Van Allen Radiation Belts
are also presented.
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2 changes: 2 additions & 0 deletions Reports/Radiation/Source/Readme.md
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# Report Source Files
This directory contains the Latex source files for reports contained within the Radiaiton Reports directory.
12 changes: 12 additions & 0 deletions Reports/Vehicle/Readme.md
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# Launch Vehicle Reports Directory
The following is a listing of reports found in this directory, along with their abstracts.

**Preview of The SpaceX Starship: General Consensus on Weights & Fuel, and Calculated ∆V**
The following memo describes characteristics of the SpaceX Starship that may be important to
the development of orbital trajectories. SpaceX has not released any finalized details on the vehicle’s
configuration as of this time, and a lot of the unofficial chatter on those details varies from week to
week. What I have accumulated here is the general consensus on certain fundamental values that
I have found in various reliable references, with those that have been repeated by more than one
source given primacy. I have also provided basic ∆V calculations based on those values, which can
act as a rough comparison when considering orbits and other options.

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# Report Source Files
This directory contains the Latex source files for reports contained within the Launch Vehicles directory.
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3 changes: 3 additions & 0 deletions launch.md
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Expand Up @@ -18,3 +18,6 @@ Verification Specification (GEVS) which represents a
3-sigma case of applied acceleration due to launch-
induced vibrations.'' [do Vale Pereira, P. et al 2020 https://digitalcommons.usu.edu/smallsat/2020/all2020/121/]

### Vehicle Reports Directory:

[Vehicle Reports](/Reports/Vehicle/Readme.md)
4 changes: 4 additions & 0 deletions radiation.md
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To go to the radiation reports directory:

[Radiation Reports](/Reports/Radiation/Readme.md)

add /Reports/Radiation/Readme.md
Radiation effects and COTS electronics reading list:

Sinclair, D., & Dyer, J. (2013). Radiation Effects and COTS Parts in SmallSats. In Small Satellite Conference (p. 12).
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