OHKLA Design/Ignition system design

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This document is part of the OHKLA Design Tasks tree.

Contents 1 Summary 2 Background 3 Features/Considerations 4 Requirements 5 Available solutions 6 Supporting material/calculations

[edit] Summary

The purpose of this design task is to design the ignition system for the OHKLA hybrid rocket engine.

[edit] Background

[edit] Features/Considerations

[edit] Requirements

[edit] Available solutions

[edit] Supporting material/calculations