Experimental Study of a Hypergolically Ignited Liquid Bipropellant Rotating Detonation Rocket Engine
| Autor: | Carl R. Hartsfield, Brandon Kan, Stephen D. Heister, Wesly S. Anderson |
|---|---|
| Rok vydání: | 2020 |
| Předmět: |
020301 aerospace & aeronautics
Materials science business.industry Mechanical Engineering Nuclear engineering Detonation Aerospace Engineering 02 engineering and technology 01 natural sciences Pressure sensor 010305 fluids & plasmas law.invention Ignition system chemistry.chemical_compound Fuel Technology 0203 mechanical engineering chemistry Space and Planetary Science law Combustion process 0103 physical sciences Rocket engine business Hydrogen peroxide |
| Zdroj: | Journal of Propulsion and Power. 36:851-861 |
| ISSN: | 1533-3876 0748-4658 |
| Popis: | A liquid bipropellant rotating detonation rocket engine was successfully test fired. The 6.5-in.-diam engine operates on a mixture of rocket-grade hydrogen peroxide and triglyme. Ignition is accomp... |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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