FO Technologies on the Moon¶
Last updated: Session 27, 2026-04-06
Summary¶
Seven technologies matured through NASA's Flight Opportunities (FO) program have operated on the lunar surface. An eighth reached the Moon but couldn't deploy. At least four more are planned for upcoming CLPS missions through 2028.
These seven technologies span three CLPS missions in 13 months (Feb 2024 – Mar 2025), covering navigation, propellant management, radiation tolerance, regolith sampling, GNSS positioning, radiation monitoring, and geophysical sounding. Together they represent the strongest evidence for FO's role in NASA's return to the Moon.
Correction history: - Sessions 1–22 counted "3 FO technologies on the Moon" (NDL, RadPC, PlanetVac). - Session 23 corrected to 6: added RFMG on IM-1, LuGRE on Blue Ghost, ARMAS on IM-2. - Session 27 corrected to 7: added SwRI Lunar Magnetotelluric Sounder (LMS) on Blue Ghost — discovered via SwRI cluster investigation. FO project 106681 (High-Altitude EM Sounding, TRL 2→5, PI Grimm) directly led to LMS, which deployed on the lunar surface March 2, 2025. First extraterrestrial magnetotellurics deployment in history.
Confirmed on the Lunar Surface (7)¶
1. Navigation Doppler Lidar (NDL) — IM-1 Odysseus, Feb 22, 2024¶
| Item | Detail |
|---|---|
| FO Projects | 91351 NASA LaRC (TRL 5→6, 2013–2019) + 106687 Psionic (TRL 4→6, 2019–2021) |
| Developer | NASA Langley Research Center → licensed to Psionic, Inc. (2016) |
| PI | Farzin Amzajerdian (LaRC); Diego Pierrottet (Psionic) |
| CLPS Mission | Intuitive Machines IM-1 "Odysseus" Nova-C lander |
| Landing | Malapert A, near lunar south pole, Feb 22, 2024 |
| Result | NDL saved the mission. Primary laser rangefinder safety switch failed pre-launch. Mission controllers reprogrammed Odysseus to use NDL as primary sensor. NDL provided 100% valid altitude/velocity data from 10 km to the surface. First commercial soft landing on the Moon. |
| Downstream $ | $15.6M tracked (Psionic NASA contracts) |
| KB Page | organizations/psionic-ndl.md |
Why it matters: This is the single strongest causal argument for the FO program. Without FO-validated NDL, the first commercial Moon landing fails. The 11-year arc from lab concept (2006) through FO testing (2013–2019) to commercial license (2016) to lunar surface (2024) is a textbook technology transfer story.
2. Radio Frequency Mass Gauge (RFMG) — IM-1 Odysseus, Feb 22, 2024¶
| Item | Detail |
|---|---|
| FO Projects | 12177 RF Mass Gauge parabolic (TRL 4→6, 2011–2020) + 91405 RF Gauging on Masten Xaero LOX tank (TRL 4→6, 2011–2020) |
| Developer | NASA Glenn Research Center |
| PI | Gregory Zimmerli (GRC, inventor of RFMG) |
| CLPS Mission | Intuitive Machines IM-1 "Odysseus" Nova-C lander |
| Landing | Malapert A, near lunar south pole, Feb 22, 2024 |
| Result | RFMG measured propellant levels throughout the mission: tank loading on the pad, translunar coast, lunar orbit insertion, powered descent, and post-landing. Data validated RFMG performance in actual lunar mission conditions. Previously flown on ISS (RRM3, 2018). |
| Publications | "Results from the Radio Frequency Mass Gauge Technology Demonstration on the Intuitive Machines Nova-C Lunar Lander" (NTRS 20240014338) |
| KB Page | organizations/grc-cryogenic-power.md |
Why it matters: RFMG addresses a fundamental problem — you can't use a standard fuel gauge in microgravity. The FO parabolic flight tests were essential for validating RFMG in reduced gravity before committing to a lunar mission. NASA's August 2024 Community of Practice webinar featured both NDL and RFMG PIs presenting "Journey to the Lunar Surface: From Suborbital Flight Testing to Moon Mission."
KB correction needed: GRC cryogenic page documents RFMG's FO heritage and ISS flight but doesn't flag the IM-1 lunar landing as a confirmed outcome. This session corrects that.
3. Radiation-Tolerant Computer (RadPC) — Blue Ghost M1, Mar 2, 2025¶
| Item | Detail |
|---|---|
| FO Projects | 91411 (TRL 5→7, 2013–2017) + 106701 RadPC@scale (TRL 6→7, 2020–2023) + 106658 biology payload reuse (TRL 7→7, 2021–2024) |
| Developer | Montana State University → Resilient Computing LLC (spinoff) |
| PI | Brock LaMeres (MSU) |
| CLPS Mission | Firefly Aerospace Blue Ghost Mission 1 |
| Landing | Mare Crisium, Mar 2, 2025 |
| Result | RadPC operated continuously for 346 hours (full lunar day) plus 5+ hours into lunar night. Returned 119+ GB of radiation/temperature data. TRL 9 achieved. One of 10 payloads, all successful. Firefly won 2025 Collier Trophy. |
| Downstream $ | $1.6M NASA CLPS award + Resilient Computing $2.79M federal contracts + spinoff |
| KB Page | organizations/msu-radpc.md |
Why it matters: Clearest academic FO → lunar surface arc. A Montana State FPGA lab project became a commercial spinoff (Resilient Computing) with its own FO project 184144 for RadPC+ RISC-V next-gen. The Dual-FO arc (university + spinoff both getting FO funding) is unique in the portfolio.
4. PlanetVac Pneumatic Regolith Sampler — Blue Ghost M1, Mar 2, 2025¶
| Item | Detail |
|---|---|
| FO Projects | 89413 PlanetVac Phase 1 (TRL 4→6, 2017–2019) + 106599 Phase 2 (TRL 5→6, 2019–2021) |
| Developer | Honeybee Robotics (Blue Origin subsidiary since 2022) |
| PI | Kris Zacny |
| CLPS Mission | Firefly Aerospace Blue Ghost Mission 1 |
| Landing | Mare Crisium, Mar 2, 2025 |
| Result | PlanetVac successfully collected, transferred, and sorted lunar regolith using pressurized nitrogen gas. Sample collection took approximately one second. Deployed by Blue Ghost's Surface Access Arm. |
| Next | P-Sampler (PlanetVac variant) flying to Phobos on JAXA MMX mission (launching 2026) — FO→Moon→Mars system chain |
| Downstream $ | $193M+ Honeybee NASA portfolio; $6.31M Blue Ghost CLPS contract |
| KB Page | topics/honeybee-planetvac-cluster.md |
Why it matters: The Masten Xombie VTVL rocket provided a uniquely realistic powered-descent test environment that parabolic flights can't simulate. Irony: Masten, which provided the FO test platform, went bankrupt in 2022 — but the technology they helped validate flew to the Moon on a different lander. PlanetVac also has the strongest interplanetary trajectory: Moon (2025) then Mars's moon Phobos (2026).
5. Lunar GNSS Receiver Experiment (LuGRE) — Blue Ghost M1, Mar 2, 2025¶
| Item | Detail |
|---|---|
| FO Project | 106593 GPS/Galileo Receiver for Human Exploration (TRL 4→5, Feb–Oct 2020) |
| Developer | Qascom S.r.l. (Bassano del Grappa, Italy) — joint NASA/ASI payload |
| PI | Oscar Pozzobon (Qascom) |
| CLPS Mission | Firefly Aerospace Blue Ghost Mission 1 |
| Landing | Mare Crisium, Mar 2, 2025 |
| Result | First-ever GNSS navigation fix on the lunar surface. LuGRE acquired and tracked GPS and Galileo signals from ~247,520 miles, setting distance records. On Mar 3, 2025, it computed the first GNSS position fix on the Moon using 4 satellites (2 GPS + 2 Galileo). Data released publicly by NASA/ASI. |
| KB Page | (previously classified as dead end — corrected this session) |
Why it matters: This was previously classified as a dead end in Session 4 ("8-month project, no description in TechPort, foreign company, no follow-on contracts found"). The FO project had zero description text and no outcome records — but the 8-month Qascom FO project in 2020 was the maturation step for the LuGRE receiver that made history on the Moon. Lesson: TechPort's empty description fields can hide the most significant outcomes. The FO project was short (8 months) and had minimal TechPort metadata, but it was the critical link between Qascom's ground-based heritage (QN400-Space) and lunar qualification.
KB correction: Reclassified from "dead end" to "Mission Infusion — confirmed." This is the largest single correction in the KB's history.
6. ARMAS Radiation Monitor — IM-2 Athena, Mar 6, 2025¶
| Item | Detail |
|---|---|
| FO Projects | 89360 ARMAS-Hi (TRL 6→7, 2017–2019) + 106715 ARMAS DM POMD (TRL 7→8, 2020–2024) + 106693 ARMAS-S (TRL 4→6) |
| Developer | Space Environment Technologies (SET), Pacific Palisades CA |
| PI | W. Kent Tobiska (SET President/Chief Scientist) |
| CLPS Mission | Intuitive Machines IM-2 "Athena" Nova-C lander |
| Landing | Mons Mouton, lunar south pole (inside crater, 250m from target), Mar 6, 2025 |
| Result | ARMAS FM11 collected ~32 hours of continuous radiation data across six regions: Earth upper atmosphere, Van Allen belts, deep space, lunar orbit, lunar landing, and lunar south pole surface. First continuous radiation measurement across the full Earth-to-Moon transit. Lander tipped on its side; ARMAS operated throughout transit and initial surface time before battery depletion. |
| Downstream $ | ~$7.9M tracked (NASA + DoD + NOAA) |
| KB Page | organizations/set-armas.md |
Why it matters: ARMAS achieved the southernmost lunar landing and surface operations ever. Even though IM-2's landing was imperfect (lander tipped), ARMAS collected its primary data during transit — the radiation environment characterization from LEO to lunar surface. The 15+ year, 10+ flight maturation chain through FO is one of the longest in the portfolio.
7. Lunar Magnetotelluric Sounder (LMS) — Blue Ghost M1, Mar 2, 2025¶
| Item | Detail |
|---|---|
| FO Project | 106681 High-Altitude EM Sounding (TRL 2→5, 2017–2019) |
| Developer | Southwest Research Institute (SwRI) |
| PI | Robert E. Grimm (SwRI, same PI as FO project) |
| CLPS Mission | Firefly Aerospace Blue Ghost Mission 1 |
| Landing | Mare Crisium, Mar 2, 2025 |
| Result | First extraterrestrial magnetotellurics deployment in 50+ years of the technique's history. LMS deployed 5 EM sensors on the lunar surface and began probing the Moon's interior to depths of up to 700 miles (two-thirds of lunar radius). Measured electric and magnetic fields to build conductivity profiles of the lunar interior. |
| Follow-on | LITMS (Lunar Interior Temperature and Materials Suite) selected for Schrödinger Basin, lunar far side — SwRI-led follow-on instrument suite |
| KB Page | organizations/swri-cluster.md |
Why it matters: This was hiding in plain sight. FO project [106681] had only 725 views and was categorized as basic geophysics research (TRL 2→5). But the TechPort library items themselves contained the tell: a press release titled "SwRI awarded lunar lander investigation contract." The FO balloon tests validated high-altitude EM sounding, which Grimm then adapted for the lunar environment. TRL gain of +3 (2→5) is one of the highest in the FO portfolio — and the technology went from TRL 2 to the Moon in 8 years. Session 27 discovery — the 4th Blue Ghost FO payload identified.
Reached the Moon, Did Not Deploy (1)¶
8. AstroAnt Mini Robot — IM-2 Athena, Mar 6, 2025¶
| Item | Detail |
|---|---|
| FO Project | 106703 Autonomous Robot Swarms for Lunar Orbit Servicing (TRL 5→6, MIT) |
| Developer | MIT Space Exploration Initiative (Ariel Ekblaw) |
| CLPS Mission | IM-2 Athena (commercial payload on MAPP-1 rover) |
| Result | AstroAnt was mounted on the MAPP-1 rover's top panel for contactless thermal diagnostics. When IM-2 tipped on landing, the MAPP rover could not deploy. AstroAnt reached the Moon but did not operate on the surface. |
FO enabled AstroAnt testing in 2021 on Zero-G Corporation parabolic flights, demonstrating mobility in simulated lunar, Martian, and microgravity environments.
Planned for Lunar Surface (4+)¶
8. Modal Propellant Gauging (MPG) — IM-3 NOVA-C, ~2026¶
| Item | Detail |
|---|---|
| FO Projects | 9 projects spanning 2014–2027 (longest continuous FO arc) |
| Developer | Carthage College (PI: Kevin Crosby) |
| CLPS Mission | Intuitive Machines IM-3, Reiner Gamma swirl |
| Status | IM-3 scheduled for second half of 2026. MPG under development for integration on Nova-C lander. Also has Airbus commercialization partnership and TechLeap $500K prize. |
| KB Page | organizations/carthage-college-mpg.md |
9. DMEN/TRN (Terrain-Relative Navigation) — CP-12, ~2026¶
| Item | Detail |
|---|---|
| FO Projects | 7 projects spanning 2011–2025 (14-year arc, including 2 canceled) |
| Developer | Draper Laboratory |
| CLPS Mission | CP-12 (ispace APEX 1.0 lander), Schrödinger Basin, lunar far side |
| Status | Draper is the mission integrator with $56.93M NASA contract. DMEN is the primary landing guidance system. Target 2026. |
| KB Page | organizations/draper-precision-landing.md |
10. JAM (Jervis Autonomy Module) — CP-12, ~2026¶
| Item | Detail |
|---|---|
| FO Project | 155243 (TRL 4→6, 2023–2027) |
| Developer | Rhea Space Activity |
| CLPS Mission | CP-12, lunar orbit relay satellite (not surface lander) |
| Status | JAM flying on CP-12 data relay satellite. Deep Impact algorithm heritage. $9.8M+ DoD contracts for GPS-denied navigation. |
| KB Page | organizations/rhea-space-activity.md |
11. SELINE (Lunar Radiation Environment) — CLPS ~2028¶
| Item | Detail |
|---|---|
| FO Projects | 5 JANUS platform projects spanning 2013–2026 (12-year arc) |
| Developer | JHU/APL (PI: H. Todd Smith / Drew Turner) |
| CLPS Mission | SELINE, selected Jan 21, 2026, landing ~2028 |
| Status | Europa Clipper PIMS Faraday cups adapted for lunar radiation environment. PI Drew Turner is Europa Clipper PIMS investigation scientist. |
| KB Page | organizations/jhuapl-janus-seline.md |
Timeline¶
2024
Feb 22 IM-1 Odysseus — NDL + RFMG (2 FO technologies)
First commercial Moon landing
NDL saves mission when primary sensor fails
2025
Mar 2 Blue Ghost M1 — RadPC + PlanetVac + LuGRE + LMS (4 FO technologies)
First fully successful commercial Moon landing
First GNSS fix on lunar surface
First extraterrestrial magnetotellurics
14 days of surface operations (Collier Trophy)
Mar 6 IM-2 Athena — ARMAS + AstroAnt (2 FO technologies; 1 couldn't deploy)
Southernmost lunar landing ever
Lander tipped; partial data collection
2026
H2 IM-3 NOVA-C — MPG (planned)
Reiner Gamma swirl
~2026 CP-12 — DMEN + JAM (planned)
Schrödinger Basin, lunar far side
First far-side CLPS landing
2028
TBD CLPS — SELINE (planned)
Lunar radiation environment for human safety
Patterns¶
Every CLPS Moon landing has carried FO-matured technology¶
- IM-1 (Feb 2024): 2 FO payloads (NDL, RFMG)
- Blue Ghost M1 (Mar 2025): 4 FO payloads (RadPC, PlanetVac, LuGRE, LMS)
- IM-2 (Mar 2025): 2 FO payloads (ARMAS, AstroAnt)
This is not coincidence — FO is structurally designed as the suborbital maturation pipeline that feeds into CLPS lunar delivery.
FO maturation arcs for lunar technologies are long¶
- NDL: 11 years (2013 FO test → 2024 Moon)
- RFMG: 13 years (2011 FO test → 2024 Moon)
- RadPC: 12 years (2013 FO test → 2025 Moon)
- PlanetVac: 8 years (2017 FO test → 2025 Moon)
- LuGRE: 5 years (2020 FO test → 2025 Moon)
- ARMAS: 8+ years (2017 FO high-altitude test → 2025 Moon)
- LMS: 8 years (2017 FO balloon test → 2025 Moon)
Mean maturation time: ~9 years from first FO test to lunar surface. The longest arcs (RFMG, RadPC) started in 2011–2013, the earliest FO projects. LuGRE is the shortest at 5 years (short FO project, mature heritage receiver).
NASA centers led 3 of 7; industry/FFRDC/academia led the rest¶
- NASA-led: NDL (LaRC), RFMG (GRC), EDS heritage (KSC — though EDS is GCD, not FO)
- Industry: LuGRE (Qascom), ARMAS (SET), PlanetVac (Honeybee)
- FFRDC: LMS (SwRI)
- Academia: RadPC (Montana State)
The "empty metadata" problem is severe¶
LuGRE's FO project 106593 had: no description, no benefits text, no outcome records, no library items. It was an 8-month project with 719 views. Without NASA's own transitions documentation externally confirming the FO→LuGRE link, this connection would remain invisible. How many other "dead end" FO projects have hidden lunar connections?
Cross-references¶
- NDL/Psionic — full NDL arc
- GRC Cryogenic & Power — RFMG and FSP thermal heritage
- Montana State RadPC — FO → ISS → CubeSat → Moon → spinoff
- Honeybee PlanetVac cluster — 5 FO projects, Moon + Phobos
- SET ARMAS — 15-year radiation monitoring chain
- SwRI Cluster — LMS geophysical sounding (Session 27 discovery)
- Carthage College MPG — 9-project arc targeting IM-3
- Draper Precision Landing — 14-year arc targeting CP-12
- Rhea Space Activity — JAM on CP-12 relay
- JHU/APL JANUS→SELINE — 12-year arc targeting CLPS 2028
- Archetypes — relevant patterns: Archetype 6 (Government Tech → Commercial Spinoff), Archetype 2 (Middle-Step Bridge)
Verification¶
| Claim | Source | Counter-query |
|---|---|---|
| 6 FO technologies on Moon | NASA FO transitions pages + NTRS papers + mission press releases | Search for CLPS payloads not listed above that have FO TechPort records |
| NDL saved IM-1 | NASA press release Feb 2024; Psionic/IM public statements | Search for claims that primary rangefinder did work |
| LuGRE = Qascom FO [106593] | NASA FO transitions page "Flight-Tested Technologies for Safety in Space Head to the Moon"; Qascom product page | Check if LuGRE receiver is a different product from the FO-tested receiver |
| RFMG on IM-1 | NTRS 20240014338; NASA Glenn press release; FO Community of Practice Aug 2024 webinar | Check whether RFMG IM-1 integration was independent of FO test data |
| AstroAnt FO heritage | NASA FO transitions page credits FO for AstroAnt 2021 testing | Check if AstroAnt parabolic testing was funded via a different mechanism |
| Every CLPS mission carried FO tech | Enumerated above | Check Astrobotic Peregrine (Jan 2024, failed) — did it carry FO tech? Psionic PSNDL was manifested on Peregrine |
Confidence: Confirmed for all 6 lunar technologies. NASA's own Flight Opportunities program documentation explicitly credits FO maturation for each.
Sample size: 3 CLPS lunar landings (IM-1, Blue Ghost M1, IM-2), 7 FO technologies manifested, 6 confirmed operating.
Open question: Astrobotic Peregrine Mission 1 (Jan 8, 2024) carried Psionic PSNDL but failed before lunar arrival (propellant leak). If counted, that's 7 FO technologies that launched toward the Moon, with 6 reaching the surface.