FO Technologies to Mars¶
Tracing every Flight Opportunities technology with a confirmed or planned connection to Mars exploration.
Created: Session 24, 2026-04-06
Last updated: Session 37, 2026-04-07
Summary¶
Flight Opportunities has 2 confirmed Mars mission infusions, 1 planned Mars-system deployment, and a deep foundation of enabling technologies that will support future Mars missions. The confirmed infusions are among the highest-value outcomes in the entire FO portfolio.
| Tier | Count | Description |
|---|---|---|
| Confirmed mission infusion | 2 | Technology flew on a Mars mission |
| Mars-system deployment (planned) | 1 | Technology deploying to Mars's moon Phobos |
| Mars heritage / indirect | 3 | Technology data cited in Mars mission design, or Mars entry TPS heritage |
| Mars-targeted active projects | 2 | Projects explicitly targeting Mars |
| Enabling foundation | ~70 | Projects listing Mars as a destination (enabling technologies) |
Tier 1: Confirmed Mars Mission Infusion¶
G-FOLD / FOALS → Perseverance Lander Vision System (Mars 2020)¶
The highest-impact planetary mission infusion in the FO portfolio.
| Field | Value |
|---|---|
| FO Projects | 12272 (G-FOLD, TRL 3→5) + 91418 (FOALS, TRL 4→6) |
| PI | JPL (G-FOLD: Aung Aung; FOALS: includes Masten Xombie flights Dec 2014) |
| What FO tested | Fuel-optimal large divert guidance algorithms on Masten Xombie VTVL rocket (2013-2014). Real free-flying vehicle with real thrust constraints — not simulation. |
| Mars mission | Mars 2020 Perseverance rover — landed Jezero Crater, Feb 18, 2021 |
| How it infused | G-FOLD algorithms + terrain-relative navigation (TRN) became the Lander Vision System (LVS). LVS photographed the surface during descent, matched it with onboard maps, identified unmapped hazards, and guided Perseverance to land within 5 meters of target — at a scientifically interesting but geographically challenging site. |
| Mission value | >$2.5B (Mars 2020 total mission cost) |
| Confidence | Confirmed — NASA explicitly credits FO testing; NASA transitions page lists LVS as FO infusion |
The Masten Xombie test platform (used for FO testing 2013-2014) later went bankrupt in 2022 — but the guidance algorithms it helped validate flew to Mars. Same irony as PlanetVac: Masten's test infrastructure enabled technologies that outlived the company.
Full page: organizations/jpl-precision-landing.md
RFMG → Perseverance CFM Analysis¶
| Field | Value |
|---|---|
| FO Projects | 12177 (RF Mass Gauge, TRL 4→6) + 91405 (sRLV integration, TRL 4→6) |
| PI | Gregory Zimmerli (NASA GRC) |
| What FO tested | RF mass gauging technique in parabolic flight (9-year arc, 2011-2020) |
| Mars connection | RF gauging data cited in Perseverance Cryogenic Fluid Management (CFM) analysis — document "kortes_perseverancecfm_tagged.pdf" in TechPort library items |
| Also deployed | ISS RRM3 demo + IM-1 lunar surface (Feb 2024) |
| Confidence | Confirmed (indirect) — Mars connection is through cited analysis, not flight hardware |
RFMG is the only FO technology to span three destinations: ISS, Moon, and Mars (even if Mars is analysis only).
Full page: organizations/grc-cryogenic-power.md
Tier 2: Planned Mars-System Deployment¶
PlanetVac → JAXA MMX Mission to Phobos (2026)¶
| Field | Value |
|---|---|
| FO Projects | 89413, 106599, 106671 (PlanetVac phases 1-3) |
| PI | Kris Zacny (Honeybee Robotics, Blue Origin subsidiary) |
| What FO tested | Pneumatic regolith sampler on Masten Xombie VTVL rocket (2013-2019) |
| Lunar deployment | PlanetVac successfully collected lunar regolith on Blue Ghost M1 (Mar 2, 2025) — sample acquisition in ~1 second via nitrogen gas blast |
| Mars-system deployment | P-Sampler (PlanetVac variant) shipped to JAXA (Feb 2023) for MMX mission to Phobos — launching 2026, landing on Phobos (Mars's larger moon), returning samples to Earth by 2031 |
| Confidence | Confirmed (planned) — P-Sampler hardware delivered to JAXA; MMX mission in pre-launch |
PlanetVac is the only FO technology with a confirmed pathway spanning Moon → Mars system. The funding chain is uniquely international: Planetary Society → SBIR → FO → CLPS (NASA) → MMX (JAXA).
Full page: topics/honeybee-planetvac-cluster.md
Tier 3: Mars Heritage and Indirect Connections¶
C-PICA / Varda — Mars Entry TPS Heritage¶
| Field | Value |
|---|---|
| FO Project | 155263 (C-PICA Tech Transfer, TRL 6→9) |
| Company | Varda Space Industries |
| Mars connection | C-PICA is derived from NASA's PICA (Phenolic Impregnated Carbon Ablator) — the Mars entry TPS used on MSL/Curiosity (2012) and Mars 2020/Perseverance (2021). Varda's FO/Tipping Point project commercializes C-PICA for Earth re-entry; the same material family protects spacecraft entering Mars's atmosphere. |
| Status | TRL 9 achieved (W-5 returned Jan 2026 with all-Varda C-PICA); $35.8M DoD+NASA tracked |
| Confidence | Suggestive — heritage connection, not direct Mars infusion from FO project |
Full page: organizations/varda-space.md
GRC FSP Heat Pipes/Spreader — Fission Surface Power for Mars¶
| Field | Value |
|---|---|
| FO Projects | 12184 (Heat Pipe Limits, TRL 4→6) + 93976 (Radial Core Heat Spreader, TRL 5→6) |
| PI | Marc Gibson (NASA GRC) — FSP lead |
| Mars connection | These projects directly support the Fission Surface Power (FSP) system, which is designed for both lunar and Mars surface operations. The heat pipes and spreaders are components of the FSP radiator system. FSP is NASA's strategy for providing reliable power during the 14-day lunar night and for future Mars surface operations. Project [93976] lists Mars as its only destination. |
| Confidence | Confirmed (foundation) — PI identity + description explicitly tie to FSP program |
Full page: organizations/grc-cryogenic-power.md
SPLICE / DMEN — Moon+Mars Precision Landing Suite¶
| Field | Value |
|---|---|
| FO Projects | 106705 (SPLICE, TRL 4→6) + Draper DMEN arc (5 FO projects) |
| What it is | SPLICE integrates multiple precision landing subsystems (TRN, hazard detection, NDL) for Artemis and future Mars missions. Destinations: Moon and Cislunar, Mars. |
| Mars connection | SPLICE is explicitly designed for Mars as well as Moon. The Draper DMEN is on the CP-12 CLPS lander (~2026), building toward Mars-capable precision landing. |
| Confidence | Suggestive — Mars targeting stated but no Mars mission selected yet |
Full page: organizations/draper-precision-landing.md
Tier 4: Mars-Specific Active Projects¶
MARS-C — Mars Atmospheric Reactor for Synthesis of Consumables¶
| Field | Value |
|---|---|
| FO Project | 184153 (TRL 4→5, active 2025-2027) |
| Lead Org | University of Texas at San Antonio |
| What it is | Electrochemical ISRU cell that converts Martian water + regolith minerals into oxygen, hydrogen, and C1/C2 hydrocarbons at Martian temperatures and pressures. Patent pending. |
| Mars specificity | Mars-only — this is designed specifically for Mars ISRU, not adaptable to Moon. |
| Status | Very early (TRL 4→5 target); no flight test yet |
IMPRESS — Iterative Mars Penetrator for Subsurface Science¶
| Field | Value |
|---|---|
| FO Project | 184149 (TRL 2→6, active 2025-2027) |
| Lead Org | Guinn Partners |
| What it is | Swarm of small-scale probes that share a shielded entry vehicle, penetrate the Martian surface, and collect subsurface science data. |
| Mars specificity | Mars-only — designed explicitly for Mars surface/subsurface investigation. |
| Status | Very early (TRL 2→6 target is ambitious); FO as early-stage validation |
Tier 5: Enabling Foundation (Mars-Destination Projects)¶
81 FO projects (19% of the ~430 total) list Mars as a destination. Most are not Mars-specific — they develop enabling technologies applicable to Mars transit, surface operations, or crew support. The major clusters:
Cryogenic Propellant Management (~30 projects)¶
The single largest Mars-enabling cluster. These projects provide the foundational data for Artemis cryogenic propellant management, which is the same challenge for Mars transit:
| Sub-area | Key PIs | FO Projects | KB Page |
|---|---|---|---|
| RF mass gauging | Zimmerli (GRC) | 12177, 91405 | grc-cryogenic-power.md |
| Modal propellant gauging | Crosby (Carthage) | 8 projects | carthage-college-mpg.md |
| Liquid acquisition devices | Conboy (Creare) | 4 projects | creare-lad.md |
| Pool boiling + chilldown | Chung (UF) | 4 projects | uf-chung-cryogenics.md |
| Pool boiling | Mudawar (Purdue) | 4 projects | mudawar-thermal.md |
| Slosh + fluid dynamics | Collicott (Purdue) | 9 projects | purdue-collicott-slosh.md |
| EHD phase separation | Khusid (NJIT) | 3 projects | njit-ehd.md |
Full synthesis: topics/cryogenic-cluster.md
ISRU / In-Space Manufacturing¶
| Project | Lead Org | Mars-Relevant Application |
|---|---|---|
| MARS-C 184153 | UT San Antonio | Mars ISRU (O₂, H₂, hydrocarbons) |
| Mango Materials 106654 | Mango Materials | Gas fermentation ISRU for biopolymers |
| Blueshift SEER 158514 | Blueshift/Outward | Solar sintering for regolith construction |
| CisLunar SMPS 158519 | CisLunar Industries | Space metal processing |
| Space Foundry 106722 | Space Foundry | Plasma jet printing for ISM |
Life Support / Crew Health¶
Mars transit requires months-to-years of life support vs. days for lunar missions. FO projects addressing this:
- Paragon COSMIC 155245 — condensate separator for ECLSS
- Teledyne HEPS 106653 — hydrogen fuel cell (lunar night → Mars power)
- Giner NFTFC 155244 — non-flow-through fuel cell
- Space Lab Technologies 106694 — thin-film hydroponics for food production
- Dehydrated RBCs 155246 — ambient-temperature blood storage
- UTS Laundry 184142 — ultrasonic clothes washer/dryer
- GRC HULK 91429 — exercise device for long-duration crews
Precision Landing & GN&C¶
Mars precision landing inherits directly from lunar precision landing development:
- SPLICE 106705 — integrated landing suite for Moon+Mars
- Draper DMEN (5 FO projects) — hazard detection for CP-12 → future Mars
- SDSU FP2DG 155236 — next-gen powered descent guidance algorithms (Moon+Mars)
- Astrobotic LiDAR 106719 — hazard detection (Moon+Mars)
Comparison: FO to Moon vs. FO to Mars¶
| Metric | Moon | Mars |
|---|---|---|
| Confirmed mission infusions | 6 (NDL, RFMG, RadPC, PlanetVac, LuGRE, ARMAS) | 2 (G-FOLD/LVS, RFMG-indirect) |
| Planned deployment | 4+ (SELINE, MPG/IM-3, Draper CP-12, etc.) | 1 (PlanetVac/Phobos via JAXA MMX) |
| Mean maturation time | ~10 years (FO test → Moon) | ~7 years (G-FOLD: 2013 FO → 2021 Mars) |
| Enabling projects | ~180 (Moon destination) | ~81 (Mars destination) |
| Mission value | IM-1 saved by NDL (priceless) | Perseverance LVS (>$2.5B mission) |
Key insight: FO's Mars contribution is narrow but extraordinarily high-value. One confirmed infusion (G-FOLD → Perseverance) justifies the entire program on expected value grounds. The pipeline from Moon to Mars is real: PlanetVac proved the concept on the Moon (2025) and is heading to Phobos (2026). The cryogenic cluster provides the foundation data that Mars transit propellant management will rely on.
Timeline: FO to Mars¶
| Year | Event |
|---|---|
| 2013-2014 | G-FOLD/FOALS tested on Masten Xombie (FO) |
| 2013-2019 | PlanetVac tested on Masten Xombie (FO, 3 projects) |
| 2011-2020 | RFMG tested in parabolic flights (FO, 9-year arc) |
| 2021 | Perseverance lands on Mars (Feb 18) — LVS uses G-FOLD algorithms |
| 2024 | RFMG reaches Moon on IM-1 (Feb) — also cited in Perseverance CFM |
| 2025 | PlanetVac collects lunar regolith on Blue Ghost M1 (Mar 2) |
| 2026 | JAXA MMX launches to Phobos with PlanetVac P-Sampler |
| 2028 | SPLICE / Draper DMEN target Moon+Mars precision landing |
| 2031 | MMX returns Phobos samples to Earth (PlanetVac P-Sampler) |
Boundary: Air Squared / MOXIE¶
Air Squared's oil-free scroll compressor is the only moving component in MOXIE on Perseverance — the instrument that first produced oxygen on Mars (Apr 20, 2021, 16 runs through Aug 2023). Air Squared has FO project 106684 (ZVCR refrigerator), but the MOXIE connection came through separate SBIR contracts. This is FO-adjacent, not FO-infused — same company and core scroll technology, different product line. See Air Squared and mission infusion boundary cases.
Cross-References¶
- FO Technologies on the Moon — companion synthesis (7 confirmed)
- Cryogenic Cluster — 30+ projects providing Mars transit data
- Honeybee PlanetVac Cluster — Moon + Phobos arc
- JPL Precision Landing — G-FOLD/FOALS → Perseverance
- Archetypes — Archetype 2 (Gov Tech → License → Mission) includes G-FOLD
- Air Squared — MOXIE boundary case (FO-adjacent Mars connection)