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HTP/PLA/KMnO4 Hybrid Rocket Engine
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Topic: HTP/PLA/KMnO4 Hybrid Rocket Engine (Read 90418 times)
Jerry Fisher
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Virginia
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Re: HTP/PLA/KMnO4 Hybrid Rocket Engine
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Reply #100 on:
12/02/2025 03:53 pm »
The enhanced burn is not due to the lower concentration of KMnO4 infused into the PLA. It is due to a 20% infill in the PLA fuel core (a mistake in the printing). In the most recent test, the O/F ratio was ~ 1.3. This is about half of theoretical. Is there an optimum infill? The capability to vary the infill for a hybrid fuel core is unique to 3D printing.
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Jerry Fisher
Full Member
Posts: 120
Virginia
Liked: 110
Likes Given: 0
Re: HTP/PLA/KMnO4 Hybrid Rocket Engine
«
Reply #101 on:
01/07/2026 02:59 pm »
This month, I worked on upgrading from my plastic solenoid valve with a mass of ~ 94 gm with a stainless steel motorized ball valve with a mass of ~ 330 gm. As soon as I add a motorized ball valve, I have transition to a Class II rocket motor.
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