CuSP MiPS

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Description

VACCO’s cold gas Micro Propulsion System (MiPS) provides attitude control and orbital maneuvering. SWRI’s CuSP program utilizes VACCO’s cold gas system to achieve highly reliable propulsion while serving as a space weather station.

The VACCO CuSP MiPS is approximately 0.3U in volume and uses four 25 mN cold gas thrusters to develop 69 N-sec of total impulse that provides 8.8 m/s of delta-V for an 8 kg CubeSat. Each thruster independently operates to perform both delta-V and ACS maneuvers through an integrated microprocessor controller.

 

Datasheet

VACCO – CuSP MiPS

Overview
NameCuSP MiPS
ManufacturerVACCO
SubsystemPropulsion
ClassificationCold Gas System
Form FactorCubeSat
Vendor Overview
Vendor NameVACCO
Vendor Websitehttps://www.cubesat-propulsion.com
Vendor LocationUnited States
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SPECIFICATIONS
SubsystemPropulsion
ClassificationCold Gas System
Form FactorCubeSat
VendorVACCO
HeritageN/A
Mass0.513 kg
Nominal Power12.0 W

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