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Ion Control System (ICS) Characterization

Completed TRL 5 (started at 4, targeting 5)

Description

The Ion Control System (ICS) is a high specific impulse (Isp), low-thrust electric propulsion that is suitable for small satellite attitude control, precision orbit control, constellation formation management, and extended low-thrust maneuvers.

Benefits

The ICS is an Electric Propulsion (EP) micro-propulsion system providing low cost, high performance (ISP and thrust precision), reliability, easy configurability and scalability for SmallSat/CubeSat. Specific benefits include:

• Low exhaust plume contamination risk

• Large input voltage range

• No high-voltage input needed

• Low power consumption

• Secondary payload compatible (inert propellant, no pressure vessels)

• Flexible impulse control

• Scalable

Details

Technology areaPropulsion Systems > Electric Space Propulsion > Electromagnetic Propulsion
ProgramCenter Independent Research & Development: GSFC IRAD (GSFC IRAD)
Lead organizationGoddard Space Flight Center, Greenbelt, MD
Start date2017-10-01
End date2020-09-30

Project contacts

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How to get involved

This is early/mid-stage (TRL 5) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

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