CLPS Lander Risk — Impact on FO Technologies¶
FO matures the technology. CLPS delivers it to the Moon. What happens when the delivery vehicle is the bottleneck?
Last updated: Session 63, 2026-04-07
The Pattern¶
Flight Opportunities validates technologies in suborbital flight — parabolic, sounding rocket, balloon, New Shepard. CLPS then provides the ride to the lunar surface for operational deployment. This two-step pipeline has produced 7 FO technologies on the Moon across 3 CLPS missions in 13 months (Feb 2024 – Mar 2025). See FO Technologies on the Moon.
But the pipeline has a single point of failure: the commercial lander. When a CLPS provider slips, cancels, or goes bankrupt, mature FO technologies sit on the shelf regardless of their readiness. The technology is not the risk — the ride is.
This page maps every FO technology with a known or likely CLPS dependency, assesses the schedule risk of each lander, and identifies which FO investments are most exposed.
CLPS Lander Status Board (as of April 7, 2026)¶
| CLPS Lander | Provider | Status | Schedule | Risk Level |
|---|---|---|---|---|
| IM-1 Nova-C "Odysseus" | Intuitive Machines | Landed (tipped) | Feb 22, 2024 | DELIVERED |
| Blue Ghost M1 | Firefly Aerospace | Landed (successful, 14 days) | Mar 2, 2025 | DELIVERED |
| IM-2 Nova-C "Athena" | Intuitive Machines | Landed (tipped) | Mar 6, 2025 | DELIVERED |
| IM-3 Nova-C "Trinity" | Intuitive Machines | Manifested | H2 2026 | MODERATE — two prior tip-overs; third attempt |
| Griffin-1 | Astrobotic | Integration | NET Jul 2026 | HIGH — Peregrine failed Jan 2024; Griffin is new design |
| Blue Ghost M2 | Firefly Aerospace | Testing (JPL, Dec 2025) | Late 2026 (far side) | LOW — M1 success builds confidence; relay sat adds complexity |
| Blue Moon MK1 Pathfinder | Blue Origin | TVAC at JSC (Feb 2026) | Q1-Q2 2026 (slipping) | MODERATE — first flight; BE-7 engine untested in space |
| Blue Moon MK1 VIPER | Blue Origin | Planning | NET late 2027 | HIGH — depends on pathfinder success + VIPER reassignment |
| CP-12 (ispace ULTRA) | Draper / ispace-US | Redesign | NET 2030 (pending NASA approval) | VERY HIGH — 4-year delay; ULTRA replaces APEX 1.0; two engine failures |
| Blue Ghost M3 | Firefly Aerospace | Planning | 2028 (Mons Gruithuisen) | MODERATE — 2+ years out |
| Blue Ghost M4 | Firefly Aerospace | Planning | 2029 (Haworth Crater) | MODERATE — 3+ years out |
FO Technologies with CLPS Dependencies¶
Tier 1 — Already Delivered to the Moon (7 technologies, 3 landers)¶
These FO technologies have completed their CLPS ride. Risk: none (delivered).
| FO Technology | FO Project(s) | CLPS Lander | Date | Result | KB Page |
|---|---|---|---|---|---|
| Navigation Doppler Lidar (NDL) | 91351, 106687 | IM-1 | Feb 2024 | Saved the mission — primary sensor failed, NDL stepped in | psionic-ndl.md |
| RF Mass Gauge (RFMG) | 12177, 91405 | IM-1 | Feb 2024 | Measured propellant through all mission phases | grc-cryogenic-power.md |
| RadPC (rad-tolerant computer) | 91411 | Blue Ghost M1 | Mar 2025 | 346 hrs lunar day + 5+ hrs lunar night; TRL 9 | msu-radpc.md |
| PlanetVac (regolith sampler) | 89413, 106599 | Blue Ghost M1 | Mar 2025 | First pneumatic regolith collection on the Moon | honeybee-poccet.md |
| LuGRE (lunar GNSS) | 106593 | Blue Ghost M1 | Mar 2025 | First GNSS fix on lunar surface (Mar 3, 2025) | qascom-lugre.md |
| ARMAS (radiation monitor) | 89360, 106715 | IM-2 | Mar 2025 | Operated through lunar surface operations; southernmost landing | set-armas.md |
| Lunar Magnetotelluric Sounder (LMS) | 106681 | Blue Ghost M1 | Mar 2025 | First extraterrestrial magnetotellurics deployment | swri-cluster.md |
Key insight: All 7 delivered technologies rode on landers that worked on the first or second attempt by their providers. Intuitive Machines tipped both times but delivered enough data. Firefly succeeded clean on M1. The pipeline works when the lander works.
Tier 2 — Manifested on Upcoming CLPS Missions (active risk)¶
| FO Technology | FO Project(s) | CLPS Lander | Schedule | Risk | KB Page |
|---|---|---|---|---|---|
| DMEN (terrain-relative nav) | 12186, 106585, 106613, 106711 | CP-12 (ispace ULTRA) | NET 2030 | VERY HIGH — 19-year arc (2011-2030); tech mature (TRL 6-7, flew NS-29 Feb 2025); lander redesign after two engine failures; pending NASA approval | draper-precision-landing.md |
| JAM (autonomous cislunar nav) | 155243 | CP-12 relay sats | NET 2030 | VERY HIGH — JAM units on CP-12 relay satellites; same lander dependency as DMEN; $750K TechFlights grant at risk | rhea-space-activity.md |
| Modal Propellant Gauging (MPG) | 94131 + 8 others | IM-3 | H2 2026 | MODERATE — test article confirmed but NOT on operational manifest; IM track record: 2 landings, 2 tip-overs; MPG has backup paths (Airbus, on-orbit refueling) | carthage-college-mpg.md |
| MoonRanger (micro-rover) | Via 14162, 96188 | Blue Ghost M4 | 2029 | MODERATE — 3 years out; CMU/Whittaker heritage; originally Masten XL-1 (bankrupt), reassigned to Firefly | cmu-whittaker-lunar-pits.md |
| SELINE (lunar radiation) | Via 106720 | Unassigned CLPS | 2028 target | MODERATE — selected Jan 2026 but no provider assigned yet; site-agnostic | jhuapl-janus-seline.md |
Tier 3 — Likely Future CLPS Customers (no confirmed manifest)¶
| FO Technology | FO Project(s) | Likely CLPS Path | Status | KB Page |
|---|---|---|---|---|
| ExoCam (landing camera) | 106700 | Orphaned — original host Masten bankrupt 2022 | Searching for new platform; TRL 4→6 achieved | zandef-deksit.md |
| SPARTA (regolith instrument) | 106611, 106730 | Competing for Artemis IV / LTV slot | No confirmed host; TRL 4→6 | jpl-sparta.md |
| FIGARO-FT (5G lunar relay) | 106617 | LunaNet architecture (needs relay host) | TRL 4→5; no confirmed CLPS host | sdsu-figaro-ft.md |
| EBDM (dust mitigation) | 184151 | Artemis surface assets | Parabolic flights summer 2026; Artemis IV DUSTER instrument | space-dust-rnt.md |
| SEER (solar sintering) | 158514 | Landing pad construction | TRL 5→6; natural CLPS payload for surface base | blueshift-outward.md |
Risk Analysis¶
The Draper/CP-12 Case Study¶
The CP-12 delay is the most dramatic illustration of lander risk:
- Draper's DMEN has been in continuous FO development since 2011. It has flown on Astrobotic Xodiac, three Blue Origin New Shepard flights, and KSC field tests. The technology is at TRL 6-7 — fully mature for lunar descent.
- ispace's lander has gone through three engine suppliers. The original engine failed. The replacement (Agile Space Industries' VoidRunner) failed to meet performance specs (May 2025). The third replacement is unnamed. ispace announced ULTRA (March 27, 2026), merging APEX 1.0 and Series 3 into a new design, pushing the schedule to NET 2030.
- Result: A 19-year technology maturation arc (2011-2030) where the last ~9 years of delay are entirely on the delivery vehicle side.
Collateral damage: Rhea Space Activity's JAM ($750K TechFlights grant) rides on the same CP-12 relay satellites. Two FO organizations' lunar deployment delayed by a single lander's engine problems.
The Masten Bankruptcy Cascade¶
Masten Space Systems went bankrupt in July 2022. Downstream effects on FO technologies:
| Impact | Detail |
|---|---|
| XL-1 CLPS mission ($66.1M) | Cancelled. Payloads scattered across other missions. |
| MoonRanger (CMU) | Reassigned: Masten XL-1 → Firefly Blue Ghost M4 (2029). ~7-year delay from original schedule. |
| Heimdall camera | Reassigned: Masten XL-1 → Firefly Blue Ghost M3 (2028). |
| ExoCam (Zandef Deksit) | Orphaned. No new host confirmed. Technology in limbo. |
| Xodiac VTVL platform | Absorbed by Astrobotic. Lost in May 2025 crash (flight 176). 3 successors funded ($17.5M). |
| M10A engine | Dormant. Absorbed by Astrobotic but not actively developed. |
Astrobotic: Dual Risk¶
Astrobotic's own FO projects (93996, 91338) matured autolanding technology that fed directly into their CLPS business. But: - Peregrine Mission 1 (Jan 2024): propellant leak → failed to land. First CLPS mission to fail entirely. - Griffin-1 (NET Jul 2026): new, larger lander design. Carrying the FLIP rover (Astrolab), not FO payloads directly. But the XL-1 payload reassignments depend on Astrobotic/Firefly succeeding.
Intuitive Machines: Persistent Tip-Overs¶
- IM-1 (Feb 2024): Tipped on landing. NDL data confirmed; RFMG data confirmed. Partial success.
- IM-2 (Mar 2025): Tipped on landing again. ARMAS data confirmed. Partial success.
- IM-3 (H2 2026): Third attempt. Carries Carthage MPG test article (unconfirmed on manifest).
IM delivers data even when tipped, but the pattern raises questions about whether payloads requiring upright operation (like MPG propellant gauging demonstrations) can get full data.
Systemic Findings¶
1. Technology maturity is not the bottleneck¶
Every FO technology in Tier 2 has reached its FO target TRL. DMEN is TRL 6-7. JAM is TRL 6. MPG has been at TRL 6 for years. The technologies are ready. The landers are not.
2. Single-lander dependency creates fragility¶
When an FO technology is manifested on one specific CLPS mission, it inherits all of that mission's risks. Draper's 14-year investment in DMEN is held hostage by ispace's engine supplier problems. Zandef's ExoCam is orphaned because its only host went bankrupt. Diversifying across multiple CLPS providers (as Honeybee has done with PlanetVac on Blue Ghost + future missions) reduces this risk.
3. Firefly is the most reliable CLPS provider for FO¶
Of the 4 CLPS providers that have attempted landings: - Firefly: 1/1 clean success (Blue Ghost M1, 14 days operations) - Intuitive Machines: 2/2 landed but tipped (partial data both times) - Astrobotic: 0/1 (Peregrine total loss) - ispace: 0/1 Japan mission (crash, Apr 2023); US mission redesigning
Firefly has 4 more CLPS missions contracted (M2-M5), making it the strongest pipeline for FO technologies seeking reliable lunar delivery.
4. Bankruptcy creates orphan technologies¶
The Masten case shows that when a CLPS provider fails, manifested technologies face multi-year delays or permanent limbo. The CLPS expansion to 21 landings (March 2026 announcement) provides more potential hosts, but reassignment takes years. ExoCam has been without a host for nearly 4 years.
5. The delivered technologies validated FO's model¶
Despite all these risks, 7 FO technologies are operating on the Moon. The pipeline works when the lander works. The 3 successful CLPS missions (IM-1, Blue Ghost M1, IM-2) carried FO payloads that collectively span navigation, propellant management, radiation tolerance, regolith sampling, GNSS, radiation monitoring, and geophysics. This is the strongest evidence that FO's suborbital-to-lunar pipeline produces results.
Timeline of FO-CLPS Delays¶
| FO Technology | Original Target | Current Target | Delay | Cause |
|---|---|---|---|---|
| DMEN (Draper) | ~2026 | 2030 | +4 years | ispace engine failures → ULTRA redesign |
| JAM (Rhea) | ~2026 | 2030 | +4 years | Same CP-12 dependency |
| MoonRanger (CMU) | ~2022 (Masten) | 2029 (Firefly) | +7 years | Masten bankruptcy → reassignment |
| ExoCam (Zandef) | ~2022 (Masten) | TBD | +4+ years | Masten bankruptcy → orphaned |
| Heimdall | ~2022 (Masten) | 2028 (Firefly) | +6 years | Masten bankruptcy → reassignment |
| SELINE (JHU/APL) | 2028 | 2028 | On track | No provider assigned yet |
| MPG (Carthage) | H2 2026 | H2 2026 | On track | IM-3 not yet slipped |
Cumulative delay across FO technologies with known CLPS dependencies: ~21+ person-years of schedule slip caused by lander issues, not technology issues.
Cross-References¶
- FO Technologies on the Moon — the 7 delivered technologies
- Gateway Cancellation Impact — different risk vector (architecture change, not lander failure)
- Draper Precision Landing — CP-12 deep dive
- Rhea Space Activity — JAM on CP-12 relay sats
- Masten Space Systems — bankruptcy cascade
- Astrobotic — Peregrine failure + Griffin-1
- Carthage College MPG — IM-3 dependency
- Honeybee PlanetVac Cluster — multi-mission diversification model
Created: Session 63 (2026-04-07)
Sources: TechPort, SpaceNews, Spaceflight Now, ispace press releases, NASA CLPS provider page, NSF Forum, Wikipedia