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Throttleable hybrid rocket engines for precise aerospace manoeuvres

open access: yes, 2019
Aim of this bachelor thesis is to describe current knowledge of hybrid rocket propulsion. Thesis describes the development of hybrid rocket engine, including its precise description of the engine.
Kříž, Tomáš
core  

Numerical analysis of flow dynamics in Hybrid Rocket Motors: the influence of thermodynamic variables on the blowing phenomenon

open access: yes
openThis thesis presents a comprehensive numerical investigation of the combustion physics in hybrid rocket engines. Hybrid rockets, which utilize a combination of solid fuel and liquid or gaseous oxidizers, offer significant advantages in terms of ...
SCRASCIA, DAMIANO
core  

Perseus Hybrid Rocket - A Student Lead Hybrid Rocketry Team

open access: yes
The Perseus hybrid rocketry team is developing a hybrid rocket system to reach a minimum altitude of 8,000 feet and a flight duration of at least one minute while capturing crucial telemetry data.
Oberg, Zane   +12 more
core  

Multimatrix Composite Materials for Rocket Nozzle Manufacturing: A Comparative Review. [PDF]

open access: yesPolymers (Basel)
Meiirbekov M   +7 more
europepmc   +1 more source

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