Fuel Ignition in HTP Hybrid Rockets at Very Low Mass Fluxes: Challenges and Pulsed Preheating Techniques Using Palladium-Coated Catalysts

Fuel Ignition in HTP Hybrid Rockets at Very Low Mass Fluxes: Challenges and Pulsed Preheating Techniques Using Palladium-Coated Catalysts

In a worldwide scenario which sees an increasing number of small satellite launches, novel mission concepts may be unlocked providing the spacecrafts with the very precise and rapid maneuvering capability that electric thrusters cannot guarantee. In this context, chemical thrusters appear to be a po...

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Bibliographic Details
Main Authors: Sergio Cassese, Stefano Mungiguerra, Veniero Marco Capone, Riccardo Guida, Anselmo Cecere, Raffaele Savino
Format: Article
Language:English
Published: MDPI AG 2024-10-01
Series:Aerospace
Subjects:
pulsed thruster
hydrogen peroxide
ignition of fuels
CubeSats
in-space fast maneuvers
Online Access:https://www.mdpi.com/2226-4310/11/11/884
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