Work

Effect of Oxidizer Injector Swirl Angle on Hybrid Rocket Performance with Additively-Manufactured Fuel

Year: 2025

Type: conference-paper

Source: AIAA Regional Student Conferences

DOI: 10.2514/6.2025-98301

Authors: Katie Rupert, Kyle King

Language: English

Topic: Rocket and propulsion systems research

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

SDG: Affordable and clean energy

Open Access status: closed

OpenAlex ID: W4413191313

FWCI:

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