High functionality at a nominal price point

Monofilament Vaporization Propulsion Thruster System (MVP)

The Monofilament Vaporization Propulsion (MVP) system draws from extrusion 3D printer technology to feed and melt Delrin fiber propellant (a common polymer). MVP then uses a low power resistojet to vaporize the Delrin propellant and provide continuous electrothermal thrust with a specific impulse of 66 s. The Delrin fiber is spooled in a cylindrical configuration surrounding a core containing all the electronics inside the package.

This technology retains performance characteristics competitive with other warm gas systems, but enables more accessibility to micropropulsion via dramatically reduced cost and the elimination of range safety concerns. A 0.93-liter sized MVP has a total impulse of 265 N-s and is a compelling option to meet many micropropulsion needs, including collision avoidance maneuvers, limited orbit raising and lowering, drag makeup, and deorbiting.

Monofilament Vaporization Propulsion Thruster System (MVP)
Propellant Options

Delrin fiber (range safety not required)

Status

Available as 1U dual fault tolerant unit with a less than 9-month lead time

Variations

Alternate form factors available with additional cost and lead time

Advantages Include:

Simplicity and safety with solid inert polymer propellant

Low-cost propulsion option

Propellant is spooled inside package and easily expanded as needed

No pressure vessel required for propellant

Compact package size as small as 1U

Well-suited for 3U or larger CubeSats

C. A. Woodruff, M. M. Parta, D. M. King, A. L. Woodruff, R. L. Burton, D. L. Carroll, Monofilament Vaporization Propulsion (MVP) Flight-like System Performance 37th International Electric Propulsion Conference Massachusetts Institute of Technology, Cambridge, MA USA, Cambridge, MA, June 19-23, 2022, DOI n/a, (2022)
C. A. Woodruff, D. L. Carroll, D. M. King, R. L. Burton, N. Hejmanowski, Monofilament Vaporization Propulsion (MVP) – CubeSat propulsion system with inert polymer propellant Small Satellite Conference, 2018, Logan, UT, USA, Aug 6-9, 2018, DOI n/a, (2018)

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