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Solid State Inflation Balloon Active Deorbiter

Completed TRL 5 (started at 3, targeting 5)

Description

The Solid State Inflation Balloon (SSIB) is a simple, reliable, low-cost, non-propulsive system for deliberate deorbit and control of downrange point-of-impact that is compatible with a full range of smallsats from 1kg to 180kg in mass, and includes built-in redundancy for enhanced reliability and safety. The gas generator contains a MEMS Solid-State Gas Generator chip and scalable array of microwells with precisely filled quantities of sodium azide. Integrated heaters decompose this into nitrogen gas to inflate a metalized polyimide balloon, allowing interactions with solar radiation pressure and the upper atmosphere to provide deorbiting drag. The total mass of the SSGG is expected to be ~10 grams, while the power consumption of the heater is ~10mW (for sequential operations of one well at a time).

Benefits

The successful development of the SSIB provides NASA a low cost technology for end-of-life or sample-return deorbit and control of downrange point-of-impact. It is compatible with a full range of masses from 1kg to 180kg, from CubeSats to MicroSats,.

Details

Technology areaEntry, Descent, and Landing > Aeroassist and Atmospheric Entry > Passive Reentry Systems for SmallSats
ProgramSmall Spacecraft Technology (SST)
Lead organizationUniversity of Arkansas, Fayetteville, AR
Start date2015-10-01
End date2017-10-17

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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