Bi-propellant Igniter (Highly Fuel Rich condition)


Duration = 00:37

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Description

Bi-propellant Igniter using ethanol and nitrousoxide as fuel and oxidezer respectively, and ignited using a glow plug. Test done as a part of design and development of a bi-propellant ignition system for Delft Aerospace Rocket Engineering's liquid Rocket Engine Deimos-F.
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