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- W1664794110 abstract "Recently, there has been interest in marrying the power and propulsion functions of military satellites in a single piece of hardware‐‐a hybrid or “ bimodal” system. This report presents a summary of a more extensive study [Kennedy, 1993] which examined how bimodal power and propulsion would enhance existing satellite missions, enable future missions, and realize cost savings for the user. Enhancements include on‐orbit maneuverability and higher payloads on‐orbit. Missions enabled by bimodal systems include a number of high‐power military applications, in addition to several commercial ones (e.g., the 100‐kWe Direct Broadcast High‐Definition Television Satellite, Global Air Traffic Control Satellites). Cost savings are accrued in three ways: (1) stepdown to smaller, cheaper launch vehicles, (2) increased satellite lifetimes, needing fewer satellites and fewer launch vehicles to perform a mission, and (3) increased satellite capabilities, enabled by the higher power available, which allows more to be done by each satellite platform. Mission architecture and system trades result in a bimodal reactor operating at a specific impulse of 770 s., a thrust level of 80 N, while providing 10 kWe for a bimodal reactor system mass of 1000 kg." @default.
- W1664794110 created "2016-06-24" @default.
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- W1664794110 date "1994-01-01" @default.
- W1664794110 modified "2023-09-23" @default.
- W1664794110 title "Summary of the Bimodal Satellite Mission Study" @default.
- W1664794110 doi "https://doi.org/10.1063/1.2950153" @default.
- W1664794110 hasPublicationYear "1994" @default.
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