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VACCO ArgoMoon Micro Propulsion System

The ArgoMoon Micro Propulsion System is a VACCO integrated hybrid system documented by NASA for the Italian Space Agency’s ArgoMoon CubeSat. It combines an ECAPS LMP-103S chemical thruster with VACCO cold-gas thrusters for spacecraft maneuvering and control. NASA records ArgoMoon’s deployment on Artemis I. That deployment establishes a mission association without proving every intended propulsion operation succeeded.

Identity

Aliases
ArgoMoon MiPSArgoMoon Micro Propulsion System
Domains
spaceflight
Identity Level
integrated-system
Kind
integrated-propulsion-system
Name
VACCO ArgoMoon Micro Propulsion System
Status
unknown

Details

Description
The ArgoMoon Micro Propulsion System is a VACCO integrated hybrid system documented by NASA for the Italian Space Agency’s ArgoMoon CubeSat. It combines an ECAPS LMP-103S chemical thruster with VACCO cold-gas thrusters for spacecraft maneuvering and control. NASA records ArgoMoon’s deployment on Artemis I. That deployment establishes a mission association without proving every intended propulsion operation succeeded.
Propellants
LMP-103SR134a

Links

Assets & Meta

Creation Time
October 17, 2026 at 14:03:59 UTC
Updated Time
October 17, 2026 at 14:03:59 UTC

Other

Sources
  • Accessed Date
    2026-10-17
    Note
    Agency survey supports the named product and stated application. Lifecycle is unknown because the survey does not establish current production or retirement status.
    Publisher
    NASA
    Title
    4.0 In-Space Propulsion — State-of-the-Art of Small Spacecraft Technology