The Journey Of The Lunar Flashlight Propulsion System From Launch Through End Of Mission

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SSC23-VI-03.pdf (3.45 MB)
Author(s)
Smith, Celeste R.
Cheek, Nathan
Burnside, Christopher
Baker, John
Adell, Philippe
Picha, Frank
Kowalkowski, Matthew
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Daniel Guggenheim School of Aerospace Engineering
The Daniel Guggenheim School of Aeronautics was established in 1931, with a name change in 1962 to the School of Aerospace Engineering
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https://hdl.handle.net/1853/74040
Abstract
The Lunar Flashlight Propulsion System (LFPS) was developed as a technology demonstration to enable the Lunar Flashlight spacecraft to reach Lunar orbit and to desaturate onboard reaction wheels. While the system produced over 16 m/s of delta-v and successfully managed momentum, variable thrust performance, most likely due to debris in the propellant flow path, kept the spacecraft from reaching the Moon. This paper details the in-flight journey of the LFPS, highlighting both successes and challenges met throughout the mission, and provides lessons learned applicable to future CubeSat missions and additively manufactured propulsion systems.
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Date
2023-08
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Text
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Paper
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