FO Mission Infusion Summary¶
The definitive inventory of Flight Opportunities technologies that infused into NASA missions, deployed to space, or transitioned to other programs.
Created: Session 25, 2026-04-06
Last updated: Session 97, 2026-04-07
At a Glance¶
| Destination | Confirmed | Details |
|---|---|---|
| Moon | 7 technologies | 3 CLPS missions (IM-1, Blue Ghost M1, IM-2), Feb 2024 – Mar 2025 |
| Crewed lunar flyby | 1 hardware + data | Artemis II (Apr 2026): CPAS parachutes (Airborne Systems) + cryo cluster data for ICPS |
| Mars | 2 | Perseverance landing (G-FOLD LVS) + CFM analysis (RFMG) |
| Earth orbit (science) | 1 | TROPICS tropical cyclone constellation (4 CubeSats, May 2023) |
| Deep space | 2 | Psyche/DSOC (VIP) + OSIRIS-REx (TAGSAM) |
| ISS deployments | 10+ | AMF, FWM, OCT, RSD, MSTIC, Exo-Brake, SPHERES/Astrobee, RFMG/RRM3, FLUTE/Axiom-1, AELISS |
| Planned | 4+ | CP-12 (Draper DMEN, Rhea JAM), IM-3 (Carthage MPG), Phobos (PlanetVac) |
| TOTAL confirmed | 23+ | Across all destinations (including Artemis II CPAS, AELISS ISS) |
Key finding: Every CLPS mission that has landed on the Moon carried FO-tested technology. The mean maturation time from FO flight test to mission deployment is ~10 years.
⚠️ Session 96 Audit (2026-04-07): Systematic audit of all mission infusion claims for aspirational vs. actual evidence. Two corrections found: 1. JPL Micro Sun Sensor [12284] (Session 95): Prox-1 descoped the sensor in 2017 before launch. TechPort library items link to intended destination, not actual flight. Downgraded from "Mission Infusion" to "Delivered but Descoped." (Micro Sun Sensor was not listed in this summary.) 2. RAVAN/VACNT [91344] (Session 96): FO sRLV flight likely never occurred (TRL stayed at 3). RAVAN CubeSat was ESTO/InVEST-funded. Libera $130M VACNTs come from NIST, not APL. Removed from Tier 5 Program Transitions.
Confirmed solid: TAGSAM (mission PI was FO co-I), TROPICS (NASA's own Transitions page documents FO link), RSD (3 FO projects with progressive TRL gains directly informed ISS module), Exo-Brake (confirmed but note: TES-7 flew on Virgin Orbit and TES-15 on Firefly Alpha, not all from ISS).
Pattern: TechPort metadata can be aspirational. Library items may link to intended missions that descoped the technology. Project descriptions may propose flights that never occurred. Always verify mission infusion claims independently.
Session 97 Extended Audit (2026-04-07): Systematic scan of all 30 FO projects with technologyOutcomes. No additional RAVAN-type corrections found — the canceled zero-TRL-gain projects are legitimately marked canceled. But discovered a third failure mode: erroneous outcome linkages — AVA [91427] and Heat Pipe [12184] have relatedProjectIds pointing to completely unrelated projects in different programs/orgs/tech areas. Also found that 4 of 6 "Advanced To" dates predate project start (recording technology history, not project outcomes). New topic page: TechPort Outcome Data Quality.
New program transition discovered: Heat Pipe → Kilopower → Fission Surface Power. FO → FO → GCD → TDM chain confirmed by TechPort outcomes and project descriptions. One of FO's strongest cases.
Tier 1: Planetary Surface (Moon + Mars)¶
Moon — 7 Confirmed (3 CLPS missions)¶
| # | Technology | FO Project(s) | Developer | CLPS Mission | Landing Date | Key Result |
|---|---|---|---|---|---|---|
| 1 | NDL (Navigation Doppler Lidar) | 91351, 106687 | NASA LaRC → Psionic | IM-1 Odysseus | Feb 22, 2024 | Saved the mission — primary rangefinder failed; NDL became primary nav sensor. $15.6M Psionic contracts |
| 2 | RFMG (RF Mass Gauge) | 12177, 91405 | NASA GRC | IM-1 Odysseus | Feb 22, 2024 | Measured propellant from launch to lunar surface. Also flew on ISS RRM3 and cited in Mars 2020 CFM |
| 3 | RadPC (Radiation-Tolerant Computer) | 91411 | Montana State → Resilient Computing | Blue Ghost M1 | Mar 2, 2025 | TRL 5→9 over 12 years; spinoff company has own FO project 184144 |
| 4 | PlanetVac (Regolith Sampler) | 89413, 106599 | Honeybee Robotics | Blue Ghost M1 | Mar 2, 2025 | Collected lunar regolith. Also flying to Phobos on JAXA MMX (2026). $193M+ Honeybee NASA portfolio |
| 5 | LuGRE (Lunar GNSS Receiver) | 106593 | Qascom S.r.l. (Italy) | Blue Ghost M1 | Mar 2, 2025 | First GNSS fix on the Moon. Previously classified as dead end in KB — corrected Session 23 |
| 6 | LMS (Lunar Magnetotelluric Sounder) | 106681 | Southwest Research Institute | Blue Ghost M1 | Mar 2, 2025 | First extraterrestrial magnetotellurics. 5 EM sensors deployed; probes lunar interior to 700 mi depth. TRL 2→5 (+3 gain). Session 27 discovery |
| 7 | ARMAS (Radiation Monitor) | 89360, 106715 | Space Environment Technologies | IM-2 Athena | Mar 6, 2025 | FM11 radiation monitoring at southernmost Moon landing site. ~$7.9M tracked |
Full page: fo-technologies-on-the-moon.md
Mars — 2 Confirmed¶
| # | Technology | FO Project(s) | Developer | Mission | Date | Key Result |
|---|---|---|---|---|---|---|
| 7 | G-FOLD/LVS (Precision Landing) | 12272, 91418 | JPL | Mars 2020 Perseverance | Feb 18, 2021 | Landed within 5m of target at Jezero Crater. FO flights tested algorithms on Masten Xombie rocket. >$2.5B mission |
| 8 | RFMG (CFM analysis) | 12177 | NASA GRC | Mars 2020 Perseverance | Feb 18, 2021 | RF gauging data cited in Perseverance cryogenic fluid management analysis. Indirect contribution |
Full page: fo-technologies-to-mars.md
Crewed Lunar Flyby — Artemis II (April 2026)¶
⚠️ Artemis Architecture Update (Feb–Mar 2026): Artemis III restructured to LEO test mission (mid-2027) — no lunar landing. First crewed lunar landing now Artemis IV (early 2028, Starship HLS). Gateway paused (Mar 2026), PPE repurposed as SR-1 Freedom Mars mission (end 2028). CLPS expanded to 21 landings. Impact on FO technologies is minimal — see Artemis III Restructuring Impact and Gateway Cancellation Impact.
FO's Artemis II contribution is primarily through hardware (CPAS parachutes) and the cryogenic data cluster informing ICPS design:
| # | Technology | FO Project(s) | Developer | Contribution | Confidence |
|---|---|---|---|---|---|
| — | CPAS Parachutes | 91422, 93997 | Airborne Systems | Manufactured Orion recovery parachutes ($13.57M contract) | Confirmed (hardware) |
| — | Cryo cluster data | 30+ projects | Multiple (Darr, Chung, Mudawar, Collicott) | Reduced-gravity cryogenic physics data informing ICPS helium pressurization design | Suggestive (design influence) |
| — | FWM PFE | 12180 | ADA Technologies | Orion fire extinguisher (Phase III SBIR for Orion) | Suggestive (unconfirmed if aboard) |
Key insight: Unlike the Moon (7 specific instruments) or Mars (specific algorithms), Artemis II's FO connection runs through company-level expertise (Airborne Systems) and the experimental data layer (cryo cluster) that gives engineers confidence in ICPS cryogenic propellant management. The crewed architecture relies on FO for validated science, not individual payloads.
Full page: fo-technologies-artemis-ii.md
Tier 2: Deep Space + Earth Science¶
Deep Space — 2 Confirmed¶
| # | Technology | FO Project(s) | Developer | Mission | Date | Key Result |
|---|---|---|---|---|---|---|
| 9 | VIP (Vibration Isolation) | 91391 | Controlled Dynamics Inc. | Psyche / DSOC | Oct 2023 | VIP stabilized DSOC laser terminal. DSOC completed Sep 2025 (307M-mi record, 13.6 Tb total). ESA interop Jul 2025 — first NASA-ESA deep-space optical link (Kryoneri Observatory, Greece, 4 links at 1.8 AU). $5.4M tracked. TRL 6→9 |
| 10 | TAGSAM (Sample Acquisition) | 12244 | Lockheed Martin | OSIRIS-REx | Sep 2023 | FO parabolic flights validated regolith sampling in microgravity. Bennu sample return ~60g |
Earth Science — 1 Confirmed¶
| # | Technology | FO Project(s) | Developer | Mission | Date | Key Result |
|---|---|---|---|---|---|---|
| 11 | Dual-Spinning CubeSat Bus | 94156 | MIT (PI Cahoy) | TROPICS (EVM) | May 2023 | FO parabolic flight → MicroMAS → TROPICS (4 CubeSats, 30-min tropical cyclone revisit) → Tomorrow.io TMS (13 launched, 11 operational, NOAA validated Jan 2026). Only FO→Earth science mission→commercial constellation |
Full page: organizations/mit-tropics-cubesat.md | Deep dive: TROPICS → Tomorrow.io Tech Transfer
Tier 3: ISS Deployments (10+)¶
Technologies that matured through FO and deployed to the International Space Station:
| # | Technology | FO Project(s) | Developer | ISS Deployment | Key Result |
|---|---|---|---|---|---|
| 12 | AMF (Additive Manufacturing Facility) | 91394 | Made in Space → Redwire | 2014 (ISS CRS-5) | First 3D printer in space. TRL 4→9. Redwire acquisition. Commercial ISS facility |
| 13 | RSD (Ring-Sheared Drop) | 91350, 94137, 106625 | RPI (PI Hirsa) | Jul 2019 | ISS National Lab facility in MSG. Amyloid/pharma research. 4 FO projects, 8-year arc |
| 14 | MSTIC (Semiconductor Manufacturing) | 155254 | Made in Space → Redwire | Feb 2024 (NG-20) | 18 semiconductor crystal samples. Redwire space manufacturing line |
| 15 | Exo-Brake (Deorbit Device) | 91382 | NASA Ames (PI Murbach) | 2013–2022 (TechEdSat ×6+) | TRL 3→8 (highest gain in FO). 87% lifetime reduction on TES-7. Note: TES-7 flew on Virgin Orbit, TES-15 on Firefly Alpha — not all were ISS deployments. TES-5/10/13 were ISS-deployed |
| 16 | SPHERES/Astrobee | 91335, 93871 | MIT (PI Saenz-Otero) | Multiple | Free-flyer robotics platform → Astrobee successor. DARPA Phoenix partnership |
| 17 | RFMG (on RRM3) | 12177 | NASA GRC | 2018 (RRM3) | Propellant gauging demo on ISS. Precursor to IM-1 lunar flight |
| 18 | FLUTE (Fluidic Optics) | 106725 | NASA Ames / Technion | Apr 2022 (Axiom-1) | Liquid polymer lenses solidified in orbit. Led to NIAC Phase I + II ($600K) |
| 19 | FWM (Fine Water Mist Fire Extinguisher) | 12180 | ADA Technologies | Dec 2015 (OA-4) | Replaced CO₂ extinguishers on ISS. First 2 of 9 PFEs launched. Phase III SBIRs for Orion. $3.4M NASA + $39M+ DoD. Confirmed Session 34 |
| 20 | OCT (Optical Coherence Tomography) | 12464 | Wyle Laboratories | ISS Investigation #1146 | Standard SANS diagnostic. Mini OCT [157621] for Artemis (TRL 5→9, 2022–2029). 6+ publications |
| 21 | AELISS (Ammonia Electrooxidation) | 91638 | UPR (PI Cabrera → UTEP) | Oct 2020 (NG-14) | ISS ammonia oxidation experiment. 2U NanoRacks module; ~70% current density decrease in microgravity; npj Microgravity 2023. ECLSS water reclamation path. Confirmed Session 55 |
Tier 4: Planned Future Deployments (4+)¶
| Technology | FO Project(s) | Mission | Target Date |
|---|---|---|---|
| DMEN (Precision Nav) | 106585, 106613, 106711 | CP-12 CLPS (Draper) | NET 2030 |
| JAM (Cislunar Autonomy) | 155243 | CP-12 CLPS relay orbit | NET 2030 |
| MPG (Modal Propellant Gauging) | 8 FO projects (Carthage) | IM-3 Nova-C | TBD |
| PlanetVac P-Sampler | 106599 | JAXA MMX (Phobos) | 2026 |
Tier 5: Program Transitions (non-mission)¶
Technologies that transitioned to other NASA programs without (yet) reaching a specific mission:
| Technology | FO Project | Transitioned To | Status |
|---|---|---|---|
| FLUTE | 106725 | NIAC Phase I [158445] → Phase II [158446] | Active (through 2026) |
| Flyover Terrain Mapping | 14162 | NIAC Phase III 96188 ($2M, first-ever NIAC Ph III, 2019); PI Red Whittaker (CMU); lunar pit exploration + Astrobotic partner | Completed |
| Gecko Gripper | 91341 | ISS Astrobee demo (Apr 2021) + OnRobot commercial product | Completed |
| ~~RAVAN CubeSat~~ | 91344 | ~~JHU/APL orbital mission (Nov 2016)~~ CORRECTED Session 96: FO sRLV flight likely never occurred (TRL stayed 3). RAVAN was ESTO/InVEST-funded, not FO. See jhuapl-vacnt-ravan.md | Removed |
| Heat Pipe → Kilopower → FSP | 12184, 93976 | GCD Kilopower [14405] → TDM Fission Surface Power [105671] (40 kWe lunar reactor, early 2030s). FO → FO → GCD → TDM. Same PI (Marc Gibson). TechPort confirms: "infused in Kilopower." $25M+ tracked. See grc-heat-pipe-kilopower.md | Active (FSP through 2028) |
| ADEPT | 91412 | GCD ADEPT/SR-1 [94041]; SR-1 sounding rocket flight Sep 2018 on UP Aerospace SpaceLoft XL met both objectives. No mission selected yet. See arc-adept-deployable-entry.md | Ready, awaiting mission |
| JANUS → SELINE | 91355 etc. | CLPS 2028 (selected Jan 2026) | Planned |
| RSD Bioreactor | 106625 | ISS campaigns (amyloid + IBP) | Active |
Cross-Cutting Analysis¶
Time from FO flight to mission deployment¶
| Technology | FO Test Year | Mission Year | Gap |
|---|---|---|---|
| TAGSAM | 2012 | 2016 (launch) / 2023 (return) | 4 / 11 years |
| G-FOLD | 2013–2014 | 2020 (launch) / 2021 (landing) | 7 years |
| AMF (ISS) | 2013 | 2014 | 1 year |
| SPHERES | 2015 | 2016+ (Astrobee) | 1 year |
| NDL | 2013–2019 | 2024 | 5–11 years |
| RFMG | 2011–2020 | 2018 (ISS) / 2024 (Moon) | 7 / 13 years |
| RadPC | 2013–2017 | 2025 | 8 years |
| PlanetVac | 2017–2022 | 2025 | 3 years |
| LuGRE | 2019 | 2025 | 6 years |
| ARMAS | 2016–2024 | 2025 | 1–9 years |
| VIP/DSOC | 2013–2018 | 2023 | 5 years |
| TROPICS | 2013–2016 | 2023 | 7 years |
| FWM (ISS) | 2012–2014 | 2015 | 1.5 years |
| OCT (ISS) | 2013–2016 | ~2017 (Investigation #1146) | 1–4 years |
Mean: ~6 years from first FO flight test to mission deployment. Range: 1 year (AMF, a rapid commercial ISS deployment) to 13 years (RFMG, a government sensor with a long maturation path).
Contribution type¶
| Type | Count | Examples |
|---|---|---|
| Primary mission-critical hardware | 4 | NDL (saved IM-1), G-FOLD/LVS (Perseverance landing), TAGSAM (OSIRIS-REx sampling), VIP (DSOC stabilization) |
| Science/measurement payload | 5 | RFMG, RadPC, ARMAS, LuGRE, TROPICS |
| ISS facility/infrastructure | 6 | AMF, RSD, SPHERES, FLUTE, Exo-Brake, MSTIC |
| ISS crew safety/health | 2 | FWM (fire suppression), OCT (SANS diagnostics) |
| Sample/regolith collection | 2 | PlanetVac, TAGSAM |
Developer type¶
| Type | Count | Examples |
|---|---|---|
| NASA center | 7 | NDL (LaRC), RFMG (GRC), G-FOLD (JPL), Exo-Brake (ARC), FLUTE (ARC), SPHERES (MIT for JSC), TAGSAM (LM for GSFC) |
| Industry | 6 | Made in Space/Redwire (AMF, MSTIC), Controlled Dynamics (VIP), SET (ARMAS), ADA Technologies (FWM), Wyle (OCT) |
| Academia | 4 | MSU (RadPC), MIT (TROPICS), RPI (RSD), Qascom (LuGRE) |
| Hybrid (NASA→commercial) | 2 | NDL (LaRC→Psionic), PlanetVac (Honeybee for JPL) |
The FO Impact Narrative¶
For a program with only 5% structured outcome tracking in TechPort, FO has produced a remarkably broad portfolio of mission infusions:
- 2 technologies that landed a rover on Mars (G-FOLD + RFMG → Perseverance)
- 7 technologies operating on the lunar surface across every CLPS landing to date
- 1 operational Earth science constellation → commercial transfer (TROPICS → Tomorrow.io TMS, 13 satellites launched, NOAA validated, $1B+ company)
- A deep space optical communications link stabilized by FO-tested hardware (DSOC on Psyche) — plus the first NASA-ESA deep-space optical interop (Jul 2025, Kryoneri Observatory at 1.8 AU)
- The first asteroid sample return using FO-validated sampling mechanics (OSIRIS-REx)
- The first commercial 3D printer in space (AMF on ISS)
- ISS fire suppression upgraded with FO-tested Fine Water Mist extinguishers replacing CO₂ units (ADA Technologies, Dec 2015)
- ISS SANS diagnostics enabled by FO-validated OCT hardware (Wyle, Investigation #1146)
The 95% gap between TechPort's structured outcome tracking and actual FO impact is the central finding of this KB. The impact is there — it's just invisible in the metadata.
Boundary Cases: What Counts as FO Mission Infusion?¶
Air Squared / MOXIE (Mars) — FO-Adjacent, Not FO-Infused¶
Air Squared's oil-free scroll compressor is the only moving component in MOXIE on the Perseverance rover — which produced oxygen on Mars for the first time (Apr 20, 2021). Air Squared also has FO project 106684 (ZVCR refrigerator, TRL 4→6, $188K). Same company, same core scroll technology platform.
Why this is NOT counted as FO mission infusion: MOXIE was developed through separate SBIR contracts from NASA JPL; the FO project (ZVCR for ISS food storage) is a different product line. FO did not contribute to MOXIE's development timeline. The connection is at the company level (Air Squared's oil-free spinning scroll), not the project level.
Why this matters anyway: Air Squared exemplifies the "SBIR Portfolio Company" archetype — one core innovation (oil-free scroll) pervades 6+ NASA application areas (Mars ISRU, cryogenic pumps, ISS food storage, spacesuits, lunar ISRU, MASC). $6.73M+ across 17 NASA contracts. FO's $188K is a small slice of a much larger NASA investment portfolio. The MOXIE connection shows how FO companies often have broader NASA impact than their FO project alone reveals.
Full page: organizations/air-squared.md
Cross-References¶
- FO Technologies on the Moon — detailed analysis of all 7 lunar technologies
- FO Technologies to Mars — G-FOLD/LVS and RFMG/CFM deep dives
- SANS Research Cluster — four FO projects attacking spaceflight vision syndrome
- ADA Technologies — FWM fire suppression ISS deployment confirmed Session 34
- Archetypes — the 14 downstream transfer patterns including "Mission Infusion"
- fo-portfolio-tracker.md — full 430-project status