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- W1966016714 abstract "Abstract Experimental investigations of the 10 N catalytic hydrazine thruster are reported. These thrusters find applications in orbit raising functions of a spacecraft. The hardware was realized and tested in a vacuum chamber (10 −3 mbar vacuum) for its performance. When tested at the design propellant supply pressure of 21.5 bar the thruster developed 10.25 N thrust at an operating chamber pressure of 16.4 bar. The thruster was also tested for off-design conditions (24, 18 and 14.5 bar propellant supply pressures) of operation to determine the steady-state performance. The chamber pressure and vacuum thrust follow more or less a linear law with the propellant-supply pressure. The thruster was also tested for its response characteristics for short (100 ms) firing durations at various propellant-supply pressures (15.5, 18.8, 22.5, 25.6 and 29.5 bar) and the experimental results are reported and discussed. The hydrazine was injected at the room temperature (300 ±5 K)." @default.
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- W1966016714 date "1985-04-01" @default.
- W1966016714 modified "2023-09-26" @default.
- W1966016714 title "Experimental investigations of the 10 N catalytic hydrazine thruster" @default.
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- W1966016714 doi "https://doi.org/10.1016/0094-5765(85)90038-4" @default.
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