“…Each coiled tube was maintained at high temperature (500 to 1400 °C) in a flowing gas environment at ambient pressures of about 1.4 atm. Gas flow rates through the test cells were approximately 100 standard cm 3 /min. Samples tested in H2, CO?, NH3, and H20 were heated to 1400 °C, while samples tested in CHd-containing environments were heated to about 500 °C to avoid Cfy dissociation.…”
This paper presents the results of an effort by the NASA Lewis Research Center (LeRC) to demonstrate the technology readiness of a long-life multipropellant resistojet for Space Station auxiliary propulsion.
“…Each coiled tube was maintained at high temperature (500 to 1400 °C) in a flowing gas environment at ambient pressures of about 1.4 atm. Gas flow rates through the test cells were approximately 100 standard cm 3 /min. Samples tested in H2, CO?, NH3, and H20 were heated to 1400 °C, while samples tested in CHd-containing environments were heated to about 500 °C to avoid Cfy dissociation.…”
This paper presents the results of an effort by the NASA Lewis Research Center (LeRC) to demonstrate the technology readiness of a long-life multipropellant resistojet for Space Station auxiliary propulsion.
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