Cassini plunged into Saturn’s atmosphere on September 15, 2017, the culmination of two decades of incredible planetary exploration. The Cassini propulsion system performed spectacularly during this lengthy mission, executing 360 propulsive maneuvers successfully. R-4D performance was impeccable during 183 main-engine burns, ranging from 1.3 seconds to 96 minutes in duration. Pressure transducer drift was negligible, latch valve back-pressure relief was nominal, and pressurization system performance was flawless, except for hard-seat prime regulator leakage early in the mission. System health checks based on helium mass calculations (helium mass budgets) demonstrated no discernible helium pressurant or propellant leakage. Premature degradation of prime MR-103H RCS thrusters was noted, but back-up RCS thrusters completed the mission successfully. Final usable propellant margins were about 25% for hydrazine and less than 1% for bipropellant.


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    Titel :

    Final Cassini Propulsion System In-Flight Characterization


    Beteiligte:

    Erscheinungsdatum :

    2018-07-09


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch





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    Initial Cassini propulsion system in-flight characterization

    Barber, T. J. / Crowley, R. T. | NTRS | 2002