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Completed TRL 9 (started at 5, targeting 9)
Objective: Flight demonstrate the JPL Hybrid Energy Storage System (low temperature, high power) using the SSTP-funded CSUNSat1 CubeSat: Environmental testing complete 9/25/15; Won CubeSat Launch Initiative Proposal so we have an expense paid launch (JPL-CSUN partnership); Selected for possible March 2016 ISS Launch. Funding proposed for these remaining activities: Support Launch Activities: Checkout of final spacecraft sequences through ground testing of the fully integrated CubeSat. Flight Operations: Experimental sequences while in flight. When characterization is complete, swap in the JPL Hybrid Energy Storage System as primary energy storage. Data Processing & Analysis: Post processing of data and validation of Hybrid Energy Storage System performance based on in flight data. Ready for infusion
Relevance & Impact: This is an enabling technology for 3 classes of Missions: 1. Landers & in situ instruments; Europa Lander; MSR (OS); 2. Sensor networks; 3. Deep Space small spacecraft. Benefits include: Cold temperature operation eliminating need of energy for battery heating; and, high discharge rate enabling high power operations such as communication and instrument operation normally not possible.
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This is a mature technology (TRL 9) — the realistic path in is usually NASA's Technology Transfer Program: licensing an existing NASA patent, or a Space Act Agreement to use NASA facilities/expertise directly. NASA also runs a startup licensing program with no upfront fee for companies formed to commercialize a specific NASA technology.
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