Thermal, Power, Sensors & Instruments — SST Portfolio Cluster¶
SST has funded 15 projects in thermal management, power systems, energy storage, sensors, instruments, and imaging. Unlike propulsion and communications — where multiple SST projects produced commercial products and flight missions — this cluster is predominantly academic research that advanced TRL within labs but rarely produced visible downstream impact. The exception is the U Michigan boomless magnetometer, which published in JGR and is being tested on a CubeSat mission.
Last updated: 2026-04-14 (session 22)
Overview¶
| Technology | SST Projects | Key Orgs | Max TRL Achieved | Flight? |
|---|---|---|---|---|
| Deployable radiators | 3 | U Dayton, Penn State, Cal State LA | TRL 5 (AMDROHP) | No |
| Cryocoolers | 2 | USU (Swenson ×2) | TRL 5 | No |
| Integrated power + thermal | 1 | UIUC | TRL 5 | No |
| Nano-enhanced power | 1 | RIT | TRL 5 | No |
| Structural batteries | 1 | U Miami | TRL 5 | No |
| Low-temp energy storage | 1 | JPL | TRL 5 | No |
| Alpha/betavoltaic | 1 | ARC + GRC | TRL 4 | No |
| Boomless magnetometer | 1 | U Michigan (Moldwin) | TRL 6 | Testing on MiTEE |
| THz receiver | 1 | ASU (Groppi) | TRL 5 | No |
| Mini FTS spectrometer | 1 | GSFC | TRL 5 | No |
| Milli-arcsecond imaging | 1 | UIUC (Kamalabadi) | TRL 6 | No |
Thermal Management (5 projects)¶
Passively Deployed Radial Radiator (155366)¶
- TRL: not reported | Period: 2024-01 → 2025-12
- Lead: University of Dayton, OH
- States: MD, OH
- Very recent project (2024-2025). Passive radial radiator for CubeSat waste heat. No documents or outcomes data available yet.
Outcome: unknown (too recent) | Confidence: speculative
Passive SMA Heat-Pipe Radiators (155365)¶
- TRL: not reported | Period: 2024-01 → 2025-12
- Lead: Penn State, PA
- States: OH, PA
- Shape-memory alloy (SMA) heat-pipe radiators that passively deploy using thermal activation. For high-intensity small spacecraft.
Outcome: unknown (too recent) | Confidence: speculative
AMDROHP — Additively Manufactured Deployable Radiator (106830)¶
- TRL: 3→5 | Period: 2020-07 → 2024-10
- Lead: California State University–Los Angeles (AANAPISI MSI)
- PI: Yen J. Kuo | Co-I: Eric Sunada (JPL), Scott Roberts
- Destination: Moon and Cislunar
- 3D-printed deployable radiator with oscillating heat pipes (OHP). Target: 50W dissipation in LEO for CubeSat form factor. Flexible OHP joints with >6 W/K conductance, 5,000 W/m/K effective thermal conductivity.
- MSI institution — one of few SST projects at a minority-serving institution.
Outcome: no-visible-outcome | Confidence: speculative
Active CryoCubeSat (91561)¶
- TRL: 3→5 | Period: 2015-11 → 2018-10
- Lead: USU | PI: Charles M. Swenson
- States: CA, MD, UT (ANNH MSI)
- Mechanical pumped fluid loop (MPFL) + pulse tube cryocooler for 75–100K detector temperatures. Additive manufacturing for embedded conformal coolant channels.
- Same PI as ATACOI [95587] — Charles Swenson runs a persistent cryogenic thermal program at USU. Two SST projects, same research thread.
Outcome: no-visible-outcome (academic) | Confidence: confirmed
Active Thermal Architecture for Cryogenic Optical Instruments — ATACOI (95587)¶
- TRL: 3→5 | Period: 2018-03 → 2022-01
- Lead: USU | PI: Charles M. Swenson
- Destination: Earth
- Advanced thermal control for cryogenic electro-optical instruments on CubeSats. Successor to Active CryoCubeSat — same PI, extended research program.
- Together with [91561], this represents a 7-year persistent USU cryogenic thermal research thread (2015–2022).
Outcome: no-visible-outcome (academic) | Confidence: confirmed
Power Systems (4 projects)¶
Integrated Power System with Active Thermal Control (91380)¶
- TRL: 3→5 | Period: 2015-10 → 2017-12
- Lead: UIUC | PI: Alexander Ghosh
- States: CA, IL
- Carbon fiber solar panels with embedded microvascular fluid channels for combined power generation, energy storage, and active thermal management. Scalable from 6U to 100 kg.
- Interesting multifunctional concept but no visible downstream.
Outcome: no-visible-outcome | Confidence: speculative
Nano-Enabled Space Power System (90693)¶
- TRL: 4→5 | Period: 2016-08 → 2018-08
- Lead: Rochester Institute of Technology | PI: Ryne Raffaelle
- States: NY, OH
- Nanomaterial-enhanced solar cells, wire harnesses, and lithium-ion batteries. Improved performance without changing physical dimensions.
Outcome: no-visible-outcome | Confidence: speculative
Lightweight Structural Battery Systems (94116)¶
- TRL: 3→5 | Period: 2016-08 → 2018-08
- Lead: University of Miami | PI: Ryan Kakkainen
- States: FL, OH
- Carbon fiber + graphitic electrodes in electrolytic polymer = structural elements that double as battery. Reduces mass by combining load-bearing and energy storage functions.
- Structural batteries remain an active research area in aerospace but have not reached flight.
Outcome: no-visible-outcome | Confidence: speculative
SmallSat Low-Temperature Energy Storage (91359)¶
- TRL: 3→5 | Period: 2013-10 → 2014-12
- Lead: JPL | PI: Sharlene Katz
- States: CA, CO
- Destination: Others Inside the Solar System
- Battery/ultra-capacitor hybrid power system for extreme low temperatures. Eliminates battery heaters for deep-space missions.
- Short 14-month project. No visible follow-on.
Outcome: no-visible-outcome | Confidence: speculative
Alpha/Betavoltaic Power Sources (10936)¶
- TRL: 3→4 | Period: 2011-08 → 2012-03
- Lead: ARC + GRC | PI: Eric Clark
- Destinations: Moon, Mars, Foundational Knowledge
- Assessment of small radioisotope power supplies using direct energy conversion (alpha/betavoltaic) for future NASA missions. Essentially a feasibility study — 7 months.
- Closed out March 2012.
Outcome: no-visible-outcome (feasibility study) | Confidence: confirmed
Sensors, Instruments & Imaging (4 projects)¶
Boomless CubeSat Magnetometer (94109)¶
- TRL: 3→6 | Period: 2016-08 → 2018-08
- Lead: University of Michigan | PI: Mark Moldwin
- States: MD, MI
- Destinations: Earth, Sun
- Quad-Mag: four magnetometer sensors on a single CubeSat card. Blind source separation algorithms identify and subtract spacecraft-generated magnetic noise, eliminating the need for a deployable boom. Science-grade measurements from inside the satellite bus.
- Published in JGR Space Physics (2023): Hoffmann, Moldwin, Strabel, Ojeda — "Enabling Boomless CubeSat Magnetic Field Measurements with Quad-Mag" (NTRS 53950636251698).
- Being tested on the MiTEE CubeSat (U Michigan Miniature Tether Electrodynamics Experiment).
- This is the highest-downstream-impact sensor project in the SST portfolio — peer-reviewed publication + CubeSat flight test.
Outcome: transitioned (published + CubeSat test) | Confidence: suggestive
Terahertz Receiver for Small Satellite Remote Sensing (94030)¶
- TRL: 3→5 | Period: 2016-08 → 2018-08
- Lead: Arizona State University (ANNH MSI) | PI: Christopher Groppi
- States: AZ, CA, OH
- Destinations: Earth, Mars, Others Inside the Solar System
- Schottky diode THz receiver repackaged using micromachining for CubeSat form factor. 10× mass/volume reduction. Enables remote sensing of water and atomic oxygen (opaque in Earth's atmosphere but scientifically critical).
- Groppi is a prominent radio astronomy instrumentalist (ASU Terahertz lab).
Outcome: no-visible-outcome | Confidence: speculative
Mini Fourier-Transform Spectrometer (106803)¶
- TRL: 3→5 | Period: 2013-10 → 2015-09
- Lead: GSFC | PI: John C. Allen
- States: MD, NC
- FT spectrometer on a chip — mid-infrared spectral signatures for atmospheric composition, mineralogy, surface processes. Eliminates bulky free-space optics and mechanical scan mirrors.
Outcome: no-visible-outcome | Confidence: speculative
Milli-Arcsecond Imaging with Smallsat Super-Resolution (95523)¶
- TRL: 3→6 | Period: 2018-03 → 2022-01
- Lead: UIUC | PI: Farzad Kamalabadi
- States: IL, MD
- Destination: Sun
- Computational diffractive optical sensing + formation flying = milli-arcsecond imaging. Unprecedented resolution using photon sieves and advanced image processing. Demonstrated in lab at TRL 6.
- NSF also awarded Kamalabadi funding for related work (Award 1936663).
- No flight mission or commercial product. Remains in academic research phase.
Outcome: no-visible-outcome (academic) | Confidence: confirmed
Cross-Cutting Findings¶
1. Academic TRL Ceiling at 5–6¶
Every project in this cluster hit TRL 5 or 6 and stopped. No thermal, power, or sensor project reached flight (TRL 7+). The exception is the Quad-Mag magnetometer, which is being tested on MiTEE but hasn't flown independently. This contrasts sharply with propulsion (5 flights) and communications (6+ flights).
2. USU Thermal Thread: 5 SST Projects, 1 Persistent Capability¶
Utah State University has 5 SST projects (the most of any university), clustered around thermal management and propulsion: - [91561] Active CryoCubeSat (Swenson, 2015–2018) - [95587] ATACOI (Swenson, 2018–2022) - [91602] ISAAC solar-panel antenna (Baktur, 2015–2017) - [106834] 3D Printed Hybrid Propulsion (Whitmore, 2020–2025) — transitioned to Marshall HLS - [95587] ATACOI (note: Swenson ran both cryo projects)
Swenson's 7-year cryogenic thermal thread is the academic analog of ARC's institutional capability building. The propulsion work (Whitmore) had visible downstream; the thermal work did not, despite similar TRL advancement.
3. MSI Representation¶
Four MSI-connected projects in this cluster: AMDROHP at Cal State LA (AANAPISI), Active CryoCubeSat at USU (ANNH), THz Receiver at ASU (ANNH), and SCALES at Cal Poly Pomona (HSI + AANAPISI). None produced flights. By contrast, the only MSI with a confirmed flight in the entire SST portfolio is SDSU (Hispanic-Serving Institution) — FIGARO-FT HAB flight Sep 2024 — and that's in the comms/PNT cluster, not thermal/power. See University Academic Outcomes.
4. No Acquisition Targets¶
Unlike propulsion and bus companies, none of the thermal/power/sensor researchers or their institutions became acquisition targets or commercial product lines. The technology stayed in labs. This may reflect the nature of the subsystems: thermal and power are integrator-dependent (you need a mission to fly them), while propulsion and comms have standalone product value.
Related Pages¶
- Smallsat Propulsion — the propulsion cluster (23 projects, 5 flights)
- Autonomy, GN&C, Computing — includes RadSat (rad-tolerant computing, flew → lunar surface)
- University Academic Outcomes — full university cluster analysis, MSI outcomes
- Archetypes — Institutional Capability Builder matches USU pattern
Org pages for this cluster¶
- U Dayton — radial radiator (2024, too recent)
- Penn State — SMA heat-pipe radiators (2024, too recent)
- Cal State LA — AMDROHP 3D-printed radiator
- U Miami — structural battery
- RIT — nano-enabled power
- U Michigan — boomless magnetometer (Moldwin)
- ASU Tempe — THz receiver (Groppi)
- UIUC — integrated power + milli-arcsecond imaging (Kamalabadi)
- USU — 5 SST projects (thermal + propulsion)