Technology Demonstration Missions (TDM)¶
Established: 2026-04-06 (session 47) | Data snapshot: 2026-04-04
Program Summary¶
TDM is NASA STMD's highest-TRL technology demonstration program — the flight demo layer above GCD. Where GCD advances technologies to TRL 5-6 in lab or ground conditions, TDM funds integrated system demonstrations at TRL 6-9, including orbital and planetary surface demos. TDM projects are significantly larger in scope and cost than GCD or FO, often involving major industry partners, multi-year timelines, and actual launch vehicles.
TDM awards are frequently structured as Tipping Point partnerships: industry-led, cost-share agreements where NASA provides partial funding and access to expertise while the company brings matching investment and commercial interest. The 2019 and 2023 Tipping Point solicitations populated much of the current TDM portfolio.
Program manager team: John W. Dankanich (Program Director), John W. Peugeot (Program Manager), Robert J. Kenny (Program Manager) — same team across virtually every TDM project, providing continuity but also creating single-point-of-failure risk if priorities shift.
Quantitative Snapshot¶
| Field | Value |
|---|---|
| Total projects | 72 |
| Active | 19 (26.4%) |
| Completed | 47 (65.3%) |
| Canceled | 6 (8.3%) |
Compared to other STMD programs: TDM is the smallest by project count (GCD=468, FO=430, SBIR=12,272), but the highest-stakes per project.
TX Distribution (all statuses)¶
| TX Area | Count | % | What it covers |
|---|---|---|---|
| TX01 Propulsion | 21 | 29.2% | Nuclear (NTP, NEP, DRACO), electric (SEP, Hall), chemical (RDRE, green propellant, cryogenic) |
| TX14 Thermal/CFM | 20 | 27.8% | Cryocoolers (20K + 90K families), CFM modeling, cryogenic storage demos |
| TX12 Manufacturing | 7 | 9.7% | OSAM/Archinaut/Joining demos, SLS composites, MISSE-X |
| TX09 EDL | 7 | 9.7% | HIAD/LOFTID, LDSD, MEDLI, TRN, ALHAT, VERS |
| TX04 Robotics | 4 | 5.6% | OSAM-1, SPIDER, HET, Restore-L |
| TX07 ISRU | 4 | 5.6% | MOXIE, OxEon Lunar Ice, Skyre LP3, Mason regolith |
| TX05 Comms | 3 | 4.2% | DSOC, LCRD, DSAC |
| TX03 Power | 1 | 1.4% | FSP only |
| Others | 5 | 6.9% | TX08, TX11, TX13, TX17, none (1 each) |
Dominant theme: Propulsion + Cryogenic = 57% of TDM. The program is fundamentally about enabling future depot-based architecture: propulsion systems (to use the propellant) and cryogenic storage/management (to store and transfer it). TX14 "thermal" is a misnomer here — in TDM context it means cryogenic propellant management infrastructure.
Two TDM Eras¶
Pre-2019: Government-led flight demos¶
Classic TDM projects with direct NASA center ownership: - MEDLI (4884) — EDL instrumentation, flew MSL 2012, TRL 9 - DSAC (4882) — deep space atomic clock, flew 2019, TRL 7 - LCRD (4795) — laser comm relay, flew 2021, TRL 7 - LDSD (4797) — supersonic decelerators, TRL 6 - LOFTID (95529) — HIAD flight demo, flew Nov 2022, TRL 7 - TRN (94147) — terrain relative nav, flew Mars 2020, TRL 7 - GPIM (11585) — green propellant mission, flew 2019, TRL 7 - MOXIE (96183) — Mars O2 ISRU, flew on Perseverance, TRL 7
These projects have the best flight-demo track record in TechPort across any program. Of the 8 listed, all flew and achieved TRL 7+ at mission completion.
2019+ Tipping Point era: Industry-led cost-share¶
The 2019 and 2023 Tipping Point solicitations shifted TDM toward commercial partnerships. NASA provides partial funding, company provides matching investment and commercial pathway.
2019 Tipping Point batch (CFM + ISRU focus): | Project | Company | Technology | Outcome | |---|---|---|---| | 116764 SpaceX CPM&T | SpaceX | >3MT LOX Starship internal transfer | Completed TRL 5 ✓ | | 116762 CDM | Lockheed Martin | LH2 transfer + long-duration storage | Active TRL 4 vs target 7 | | 116758 LEAPFROG/LEAP | ULA | LH2 transfer on Centaur V | Active TRL 4 vs target 7 | | 116757 LOXSAT 1 | Eta Space | Complete LOX CFM system in orbit | Active TRL 4 vs target 7 | | 156385 PRO-TP | Blue Origin | Lunar ISRU LO2/LH2 liquefaction | Completed TRL 4 (missed 6) | | 156386 Lunar Ice Processing | OxEon | Lunar ice-to-propellant electrolysis | Completed TRL 5 | | 156387 LP3-TP | Skyre | H2/O2 propellant plant | Completed TRL 5 | | 156388 Coupler | SpaceX | Cryo fluid coupling for Starship | Completed TRL 5 | | 156389 QD Coupling | Aerojet | Electrically actuated cryo coupling | Completed TRL 5 |
2023 Tipping Point batch (construction + joining + HIAD focus): | Project | Company | Technology | Outcome | |---|---|---|---| | 156390 Joining Demos | Lockheed Martin | In-space structural/electrical joining | Active TRL 4→8, Oct 2026 | | 156391 VERS HIAD | ULA | 10-meter HIAD for Vulcan engine reuse | Completed TRL 4 (ended Nov 2025) | | 156392 Mason | Redwire Space | Microwave sintering lunar regolith | Completed TRL 4 (missed 6) |
The Cryocooler Family (6 active MSFC/GRC projects)¶
TDM is running a focused cryocooler maturation campaign targeting two temperature regimes critical for propellant storage:
20K class (liquid hydrogen / liquid helium temperatures): - 158564 20W/20K RTB Cryocooler — GRC, TRL 5→6, ends Sept 2026 - 158524 Alternative Cryocooler — MSFC, TRL 4→6, 2024-2032 (develops alternatives to Creare RTB)
90K class (liquid oxygen / liquid nitrogen temperatures): - 158620 150W/90K RTB — GRC, Completed TRL 5 (Dec 2024) - 184510 30W/90K RTB — MSFC, TRL 4→6, 2025-2028 (SBIR Phase III scaled down from 150W) - 158524 Alternative Cryocooler — covers both 20K and 90K
Support hardware: - 184511 Cup Recuperator — MSFC/Creare, TRL 4→6, 2025-2026 (novel fabrication for RTB heat exchangers) - 158657 90K Cryocooler Electronics — MSFC, TRL 3→6, ends Nov 2026
The two target temperatures map directly to the cryogenic propellants: 20K for LH2 storage, 90K for LOX storage. This is infrastructure for the lunar propellant depot — store LOX and LH2 separately, transfer both. The cryocooler program is not exotic science; it's building flight-ready hardware for operational lunar logistics.
Creare LLC appears in multiple entries: They built the 150W/90K RTB (legacy fabrication). MSFC is developing new Cup Recuperator fabrication to address manufacturing defects from the Creare process.
CFM Modeling Portfolio [158415]¶
The CFMPP Modeling Portfolio (GRC, Active 2021-2030, 7,872 views — highest in TDM) is a separate TDM project developing CFD and nodal models for cryogenic operations: self-pressurization, mixing, autogenous pressurization, chilldown, boil-off. It runs to 2030 — longer than most TDM flight projects. This is the computational backbone that the hardware projects (CDM, LEAPFROG, LOXSAT 1) depend on for design and analysis.
Nuclear Propulsion: Four Projects, All Terminated at TRL 3¶
The full NTP/nuclear propulsion termination chain in TDM:
| Project | ID | TRL | Period | Outcome |
|---|---|---|---|---|
| Nuclear Thermal Propulsion TDM | 158561 | 3 vs target 5 | 2020-2025 | Completed/Closed |
| Nuclear Electric Propulsion TDM | 158369 | 3 vs target 5 | 2022-2025 | Completed/Closed |
| DRACO (NTP demo with DARPA) | 105665 | 3 vs target 6 | 2023-2025 | Completed/Closed |
| Crosscutting Fission [bridge] | 183451 | 3 vs target 4 | 2025-06 to 2025-12 | Closed Out Dec 2025 |
The Crosscutting Fission [183451] was a 6-month bridge project after the three major terminations, focused on "risk reduction and regulatory pathfinding." It closed at TRL 3 (missed TRL 4 target). The project has one library item — a photo of the Reactor Engineering Development Unit (REDU) cold flow test hardware — confirming they built real hardware before the programs ended.
The REDU cold flow test (image from TechPort library item, [183451]). A circular arrangement of fuel element tubes in a metallic housing, mounted on a test stand. Cold flow = propellant flow simulation without nuclear fuel. Hardware exists; regulatory and budget pathway does not.
The states list for [183451] (AL, ID, NM, OH, TN, VA) maps to: MSFC (AL), INL (ID), LANL or Sandia (NM), GRC (OH), ORNL (TN), LaRC (VA) — the full national nuclear laboratory network was involved. The termination closed this entire network simultaneously.
Lunar Surface Construction: Consistent TRL Miss Pattern¶
Three separate TDM/GCD Tipping Point programs targeting lunar regolith construction, all failed to reach TRL 6:
| Program | ID | Company | Technology | TRL actual vs target |
|---|---|---|---|---|
| MMPACT | 116319 | ICON Technology | VMX laser vitrification | 4 vs 6 |
| Mason | 156392 | Redwire Space | Microwave sintering | 4 vs 6 |
| Brickbot Phase II (SBIR) | 154728 | Astroport | Induction furnace-nozzle | 6 vs 6 ✓ |
The only program to hit TRL 6 was Astroport's narrow SBIR: the induction furnace-nozzle subsystem in isolation. Both GCD (MMPACT) and TDM (Mason) full-system programs stalled at TRL 4.
Note: Mason (Redwire Space) and MMPACT (ICON/BSAM) share technology overlap. Redwire acquired Blue Star Advanced Manufacturing (BSAM), which was a MMPACT microwave sintering partner. Mason is effectively Redwire/BSAM's standalone lunar construction program — yet both independently missed TRL 6. This is not a single-company failure; the entire microwave sintering approach for lunar regolith construction appears to face unresolved challenges at TRL 4→5.
See topics/lunar-surface-construction.md for the full ecosystem analysis.
Active TDM Portfolio (19 projects, April 2026)¶
| Project | ID | Lead | TX | TRL | Target | End |
|---|---|---|---|---|---|---|
| RDRE | 158559 | GRC | TX01 | 3 | 5 | 2028-09 |
| FSP | 105671 | GRC | TX03 | 4 | 8 | 2028-09 |
| SEP | 13075 | GRC | TX01 | 4 | 8 | 2029-09 |
| OSAM-1 | 105676 | GSFC | TX04 | 5 | 9 | 2026-09 |
| Joining Demos | 156390 | Lockheed | TX12 | 4 | 8 | 2026-10 |
| CDM | 116762 | Lockheed | TX14 | 4 | 7 | 2026-04-30 |
| LEAPFROG | 116758 | ULA | TX14 | 4 | 7 | 2026-09 |
| LOXSAT 1 | 116757 | Eta Space | TX01 | 4 | 7 | 2027-04 |
| CFMPP Modeling | 158415 | GRC | TX14 | — | — | 2030-09 |
| RFMG NextGen | 158537 | GRC | TX14 | 4 | 5 | 2028-11 |
| 20W/20K Cryocooler | 158564 | GRC | TX14 | 5 | 6 | 2026-09 |
| 90K Cryocooler Electronics | 158657 | MSFC | TX14 | 3 | 6 | 2026-11 |
| Alt Cryocooler | 158524 | MSFC | TX14 | 4 | 6 | 2032-02 |
| Two Stage Cooling | 158365 | MSFC | TX14 | 4 | 5 | 2030-08 |
| Low Leakage H2 Valves | 158656 | MSFC | TX14 | 4 | 5 | 2026-12 |
| 30W/90K Cryocooler | 184510 | MSFC | TX14 | 4 | 6 | 2028-10 |
| Cup Recuperator | 184511 | MSFC/Creare | TX14 | 4 | 6 | 2026-09 |
| Decreasing Uncertainty Cryo | 158583 | GRC | TX14 | 3 | 5 | 2029-03 |
| CryoFILL | 158467 | GRC | TX13 | 4 | 5 | 2026-09 |
Of 19 active TDM projects, 12 are cryogenic/thermal. The active TDM portfolio is overwhelmingly a cryogenic infrastructure buildout.
OSAM-1 flagged: TRL 5 vs target 9, Active through Sept 2026. No launch manifest publicly known. The program would need to go from TRL 5 to TRL 9 in 6 months, which is impossible without a flight already scheduled and executing. This is either a TRL data lag (hardware is further along than TechPort shows) or the program will end without completing its primary objective.
April 30, 2026 closeout watch: CDM [116762] ends April 30. Check for outcome path, TRL final record, and any closeout documentation.
Flight-Demo Success Rate¶
Of TDM Completed projects that targeted TRL 7+:
| Project | TRL achieved | Mission |
|---|---|---|
| MEDLI 4884 | 9 | MSL, flew 2012 |
| GPIM 11585 | 7 | Dedicated cubesat, flew 2019 |
| DSAC 4882 | 7 | Hosted on STP-2, flew 2019 |
| TRN 94147 | 7 | Mars 2020, flew 2020 |
| DSOC 93851 | 7 | Psyche, flew 2023 |
| LCRD 4795 | 7 | STPSat-6, flew 2021 |
| LOFTID 95529 | 7 | Dedicated, flew Nov 2022 |
| RFMG 105674 | 7 | Blue Ghost CLPS, flew Feb 2025 |
Older TDM pre-2019 = very high flight success rate. This is the program's track record. The Tipping Point era (2019+) is producing mixed results: SpaceX CPM&T succeeded (TRL 5 target hit), but CDM/LEAPFROG/LOXSAT 1 are at TRL 4 vs target 7, and Mason/Blue Origin PRO-TP both completed at TRL 4 vs targets of 6.
Canceled Programs (6)¶
| Project | Reason | TRL at cancel |
|---|---|---|
| 10937 Cryo Propellant S&T | Redirected to ground testbed | 5 |
| 105672 FROST/ICEE | DLR decision, COVID | 6 |
| 105673 OSAM-2 | Budget, Made in Space bankruptcy | 5 |
| 93967 Green Propellant Thruster | Aerojet, canceled after GPIM | 7 |
| 4789 Solar Sail Demo | Superseded | 5 |
| 52900 THOR HIAD | Superseded by LOFTID | 4 |
Cancellations at TRL 5-7 represent sunk cost without a flight demo. The OSAM-2 (Made in Space) cancellation is particularly notable — Made in Space filed for bankruptcy during the project.
Related Pages¶
- programs/gcd.md — GCD is the lower-TRL precursor; TDM is the flight demo layer
- topics/fission-surface-power.md — FSP TDM deep-dive
- topics/cfm-cluster.md — CFM TDM flight demos (CDM, LEAPFROG, LOXSAT 1, RFMG, SpaceX)
- topics/propulsion-theme.md — TX01 context
- topics/lunar-surface-construction.md — Mason + MMPACT + Brickbot TRL miss analysis
- topics/tx09-edl.md — HIAD/LOFTID lineage
- topics/tx14-thermal-management.md — Cryocooler cluster context
- topics/in-space-semiconductor-manufacturing.md — OSAM-2 canceled context (Made in Space)
Open Threads¶
- OSAM-1 [105676] Sept 2026 deadline — TRL 5 vs target 9. Will it launch? PM: Elizabeth Park (betsy.park@nasa.gov). Check for program status updates and potential cancellation.
- Lockheed Joining Demos [156390] Oct 2026 deadline — TRL 4→8. Full ecosystem mapped (session 48): SMART-C + FABORM ACOs were precursor work; scope = structural+electrical+fluid joining. Prediction: will close at TRL 5–6, not 8 (same TDM pattern). Full topic page: topics/isam-joining.md.
- CDM April 30 closeout — Lockheed, LH2 transfer, TRL 4 vs target 7. Post-closeout: will there be a successor or will CDM's work feed LEAPFROG?
- Cryocooler family completion (Sept-Dec 2026) — 20W/20K, Cup Recuperator, and 90K Electronics all end within 3 months of each other. These should produce hardware deliverables. Will TRL advance?
- NTP regulatory pathway — [183451] focused on "regulatory pathfinding" before closing at TRL 3. What regulatory framework exists for NTP ground testing? This is the barrier — not the technology.
- Mason closeout documents — [156392] ended March 2026, no library items. Any closeout documentation or outcome path will clarify whether TRL 4 is a hard stop or a data lag.