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- W2317232575 abstract "The environmental control systems of manned spacecraft will generate waste gases that can be useful for propulsion. Electrothermal thrusters using these gases can provide the impulse necess a ry for spacecraf t control and drag makeup. One promising biowaste thruster design uses a vortex heat exchanger. A coaxial wire-wound heater element i s contained within a cylindrical cavity. The propellant i s injected tangentially and spirals radially inward with high tangential, but low radial, velocity. around and through the heater element pr ior to expulsion through a conventional nozzle. The thruster is described and performance data for several propellants, including carbon dioxide and methane, a r e presented. The propellant is heated by passing" @default.
- W2317232575 created "2016-06-24" @default.
- W2317232575 creator A5002259614 @default.
- W2317232575 date "1970-08-16" @default.
- W2317232575 modified "2023-09-25" @default.
- W2317232575 title "Electrothermal thruster performance with biowaste propellants" @default.
- W2317232575 cites W2039745546 @default.
- W2317232575 doi "https://doi.org/10.2514/6.1970-1161" @default.
- W2317232575 hasPublicationYear "1970" @default.
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