Index

This website contains the knowledge acquired during the research and development of a hybrid rocket by the University of Padua students' team.

Documentation Technology

These pages are written in CommonMark, and thanks to MkDocs they support also LaTeX-style math formulas.

\[ c^* = \frac{I_sg_0}{C_F} = \frac{c}{C_F} = \frac{\sqrt{kRT_1}}{k\sqrt{(\frac{2}{k+1})^{\frac{k+1}{k-1}}}} \]

Documentation Layout

The knowledge will be divided based on the field of application.

- subsystems
  - propulsion
    - tank
    - lines
    - valve
    - injection
    - combustion chamber
    - nozzle
  - recovery
  - on board electronics
  - structures
  - aerodynamics
  - payload
- mission phases
  - mission plan
  - preliminary design
  - test campaign
  - critical design
  - launch campaign
  - competition