Initial research on thermal decomposition of 98% concentrated hydrogen peroxide in thruster-like conditions
| Autor: | Kiran Mohan, Grzegorz Rarata, Lukasz Mezyk, Jan Kindracki, Zbigniew Gut |
|---|---|
| Jazyk: | angličtina |
| Rok vydání: | 2022 |
| Předmět: |
Materials science
Computer Networks and Communications Nuclear engineering Thrust Propulsion Biomaterials chemistry.chemical_compound Satellite thruster Hydrogen peroxide Thermal decomposition Civil and Structural Engineering Fluid Flow and Transfer Processes Mechanical Engineering Chemical process of decomposition Metals and Alloys Engineering (General). Civil engineering (General) Green propellants Electronic Optical and Magnetic Materials Chamber pressure chemistry Hardware and Architecture Transient (oscillation) Current (fluid) TA1-2040 HTP |
| Zdroj: | Engineering Science and Technology, an International Journal, Vol 31, Iss, Pp 101054-(2022) |
| ISSN: | 2215-0986 |
| Popis: | The current research is focused on investigating the possibility of harnessing the thermal decomposition of highly concentrated Hydrogen Peroxide 98% i.e., utilizing a decomposition process initiated and maintained solely by a temperature source for low thrust propulsion system applications. This early study investigates the influence of the initial temperature of the heater, power input condition and chamber pressure on the behaviour and stability of the prototype thruster. While it is still too early to conclude on the practicality of the research it demonstrates that a stable configuration with good transient start-ups times is indeed achievable. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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