Skip to content

Arizona State University — Tempe

SST org page for Arizona State University (ASU), Tempe, AZ. Hispanic Serving Institution (HSI).

Last updated: 2026-04-14 (session 18)


SST Footprint

Project PI Period TRL Outcome
106810 DORA — Deployable Optical Receiver Aperture Daniel V. Jacobs 2020–2024 3→7 flew (ISS deploy Oct 8, 2024)
94030 THz Receiver for CubeSat Remote Sensing Christopher E. Groppi 2016–2018 3→5 no-visible-outcome

Two independent PIs, two independent labs, two unrelated technologies. DORA is optical communications; THz Receiver is submillimeter-wave instruments. The only connection is ASU as institutional home.


DORA — Deployable Optical Receiver Aperture

The Technology

A novel CubeSat-form-factor deployable optical receive system for inter-spacecraft communications: - 1 Gbps optical data rates at 1,000–10,000 km range - ≤10–20° pointing accuracy (vs. arcsecond-level for traditional optical comms) — DORA's large collecting area relaxes pointing requirements dramatically - Built with COTS components (low cost) - Designed for swarm crosslinks, constellation communications, and surface-to-orbit links (LunaNet concept) - 3U CubeSat form factor

Flight History

  • ISS deploy: October 8, 2024 (launched on SpaceX CRS-31, August 2024)
  • 56-day orbital lifetime — extreme Solar Cycle 25 activity caused rapid atmospheric drag. Reentered after 54 days.
  • Pointing system commissioning took ~1 month. Blown LNA at ASU ground station added delay.
  • Optical comms experiment curtailed — with only ~1 week before predicted reentry, attitude control commissioning was cut short and radio payload activated.
  • Radio Background Experiment (RBE1) succeeded — VHF spectrometer mapped 2–4 meter radio band, identified quiet zones. Power measurements confirmed correct spectrometer operation and excellent signal chain stability.
  • Data collected via SatNOGS network — high-speed downlink offline due to ASU ground station reception issues.
  • SmallSat 2025 paper on orbital decay rate analysis under high solar activity.

Assessment

DORA is a partially successful flight. The spacecraft operated, the radio science payload worked, but the primary optical communications experiment was not fully demonstrated due to the compressed 56-day timeline. The technology (TRL 3→7 per TechPort) was validated through ground testing and integration; the on-orbit demo was truncated by external factors (solar activity) and ground segment issues (blown LNA).

Architectural significance: DORA's relaxed pointing requirement (10–20° vs. arcseconds) is a genuine innovation for CubeSat optical comms. If proven on orbit, it would remove the biggest barrier to smallsat laser crosslinks — the need for expensive, heavy, power-hungry fine pointing systems. The concept remains valid despite the truncated demo. Confidence: confirmed (ISS deploy, SmallSat 2025 paper, SatNOGS data collection).

DORA in Context

DORA sits in the SST optical communications lineage alongside: - OCSD 11587: 200 Mbps downlink (Aerospace Corp, 2012–2018) → TBIRD - TBIRD (PTD-3) 106821: 200 Gbps world record (2022) - CLICK 94065: Laser crosslinks (MIT, flew 2022, B/C NET Q2 2026) - MOCT 94153: Pulse modulator for crosslinks (UF Conklin)

DORA's unique contribution: large-aperture, lax-pointing optical receiver. Complementary to CLICK's precision pointing approach.


THz Receiver — Submillimeter Remote Sensing

The Technology

Micromachined Schottky diode receivers for the 520–600 GHz terahertz band: - Reduced mass and volume by >10× compared to state-of-the-art - Targets: water and atomic oxygen detection (astrophysics, planetary science, Earth science) - TRL 3→5 in 2 years

PI: Christopher Groppi

  • ASU School of Earth and Space Exploration, experimental astrophysicist
  • Runs "Groppi Labs" — THz/millimeter/submillimeter technology
  • JPL collaboration: TeraCube project Co-I (JPL-led). Groppi's TechPort email is @jpl.nasa.gov, suggesting a split appointment or close collaboration.
  • Focus: imaging arrays of THz spectrometers for ground-based and suborbital telescopes
  • No visible downstream from the SST project specifically, but Groppi continues active THz research

Assessment

Standard academic instrumentation development. TRL 3→5, no flight, no commercial product. The technology serves niche astrophysics applications (star formation, interstellar medium) with small addressable markets. Groppi's JPL connection provides a pathway for future mission instrument proposals but no SST-specific transition confirmed. Confidence: confirmed (no downstream).


Institutional Notes

  • MSI designation: ASU-Tempe is classified as HSI (Hispanic Serving Institution) on DORA and AANAPISI (Alaska Native/Native Hawaiian) on THz Receiver. Both diversity-serving designations.
  • JPL collaboration: Both projects list California as a state — JPL is the external partner on DORA and the institutional connection for Groppi.
  • Student involvement: DORA was built and operated by amateur radio enthusiasts and undergraduate students at ASU. Avionics designed by undergrads. This distinguishes DORA from most SST missions (typically PI/postdoc-built).
  • ASU Interplanetary Initiative — university-wide program supporting space research; DORA featured prominently.

Publications

  • IEEE Aerospace Conference (2022): "Development of a Deployable Optical Receive Aperture" (Jacobs et al.)
  • IEEE Aerospace Conference (2024): "Ground Terminal Evaluation for DORA" — gimbal pointing and beam divergence results
  • IEEE Aerospace Conference (2025): "Integration and Delivery of the DORA CubeSat" (pre-launch)
  • SmallSat Conference (2021): "Creating Reliable Software Systems for the DORA CubeSat"
  • SmallSat Conference (2025): "Effect of High Solar Activity on the Orbital Decay Rate of the 3U CubeSat DORA"
  • NTRS 20230005792: "Development of a Deployable Optical Aperture"
  • MIT thesis: "Ground Station Mixed-Signal PCB and SFP Ethernet-to-Optical Connector for DORA" (MIT student contribution)

Cross-References


Key Takeaway

ASU Tempe has one clear SST story: DORA's innovative lax-pointing optical receiver flew but was curtailed by solar activity. The 56-day orbital lifetime is the SST portfolio's first flight significantly impacted by external environmental factors — a cautionary tale for ISS-deployed CubeSats during solar maximum. DORA's technology concept (large aperture, relaxed pointing) remains architecturally significant and complementary to precision-pointing approaches like CLICK. The THz Receiver is standard academic instrumentation with no SST-specific downstream.