Project Hybrid I
Motor Documentation
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Components of hybrid motor before flight. Shown is the nitrous oxide injector, (upper left corner) Nitrous Oxide tank fitting (gold piece, middle-left), the injector bulkhead (blue piece, lower-left), the graphite nozzle (black piece, middle), and the combustion chamber (blue piece lower right corner)
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Hybrid motor test fire set-up. The venue is immediately behind the project space building. MASA constructed a firing stand for the motor, which was built in order to capture the full force of the rocket test, and also to maximize security for club members
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Side view of rocket motor assembly prior to test fire. The nitrous oxide tank is seen hooked up to the fuel cell.
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Hybrid I rocket during test fire
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