ArchivedThis is the Foundation’s public site as it stood to 2026, retained under DAYBOOK and no longer maintained. Figures and programme states are correct as at their publication date. Return to the current site.
The Mars FoundationEstablished 2000 · Non-profit NP-2000-41187
Programmes

Twelve programmes of record, six of them still open

A programme is a multi-year commitment with a charter, a lead, a budget and — since 2004 — a written end condition. It is the unit the Foundation plans in. Grants sit inside programmes; instruments come out of them.

12 opened since 19696 open · 6 closedSums in millions of credits
Register

The whole register, in the order it was opened

Programmes of record, 1969 to date
CodeDiv.ProgrammeOpenedClosedStatusSpend
LODESTONEINSLunar-surface instrumentation19691983closed11
MERIDIANCOMAtmospheric circulation modelling19881997closed12
LATTICECOMMemory density and error correction19891997closed7
PLUMBLINESURSurface site survey20042021closed61
WELLHEADSURSubsurface hydrogen and hydration20062019closed14
GRAVELSURRegolith mechanics20092020closed9
CANOPYSURDust opacity and deposition2011—open8
KILNMATIn-situ materials and sintering2014—open22
HEARTHSTONELIFClosed-loop life support2015—open38
DAYBOOKARCArchive and publication2018—open4
LONGBOATPROCrewed transfer vessel2022—open116
TENDERPROLogistics and launch cadence2023—open31
Total programme spend, all eras, including committed LONGBOAT333.0

LODESTONE, MERIDIAN and LATTICE predate the Foundation and were given programme numbers retrospectively by the archive in 2001. Their sums are restated in credits at constant 2000 value.

Open

Currently funded

CANOPY · SUR

Dust opacity and deposition

Column opacity, deposition rate on optical and radiating surfaces, and the storm-onset statistics that every power budget depends on. The oldest open programme, because the dust has not stopped.

Opened 2011Dr Gideon Sarr
KILN · MAT

In-situ materials and sintering

Sintering regolith simulant into structural slab at power levels a surface plant could actually supply. First 400 × 400 mm slab in 2016 at 1.2 kW; qualification slab for a landing pad in 2024.

Opened 2014Dr Zhao Wenyi
HEARTHSTONE · LIF

Closed-loop life support

Ground-based closed ecology at the Cold Lab. It began by deliberately repeating a 1964 failure in order to calibrate a modern scrubber against it, and has since run 623 days closed with four occupants.

Opened 2015Dr Anselm Vogt
DAYBOOK · ARC

Archive and publication

The Foundation’s own archive, and the machinery that keeps the publication covenant honest: every funded result, every negative result, every retracted result, with a median of forty-one days from acceptance to open publication.

Opened 2018Naomi Vance
LONGBOAT · PRO

Crewed transfer vessel

The vessel. A reactor-electric transfer stage, a truss, tankage, a pressure hull for six and a water shield forward — 68.4 m overall, assembled in orbit from articles built at the Aldern Works. Construction of the first hull was authorised for 2027.

Opened 2022Tiago Mendes-Ruiz
TENDER · PRO

Logistics and launch cadence

The unglamorous half of LONGBOAT: cargo stages, manifests, a launch cadence tied to the transfer windows, and the surface plant that has to be working before anybody is asked to live in it.

Opened 2023Dr Nour Habib
Closed

Finished, and closed rather than extended

Six programmes have been closed. Four reached their charter end condition; two were closed on schedule because the decade they were funded for had ended. None was closed for failure, and the Foundation notes that this is a statement about its charters rather than about its luck.

LODESTONE · INS

Lunar-surface instrumentation

Three tranches of instruments carried on lunar surface payloads operated by others: corner-cube ranging arrays, short-period seismometers, and dust adhesion monitors. Named retrospectively in 2001; at the time it was three separate endowments with one condition in common.

1969–1983Dr Teodora Ilic
MERIDIAN · COM

Atmospheric circulation modelling

A general circulation model of the Martian atmosphere, run for nine years on machines that were never quite adequate. Its purpose was narrow: to decide, from the air alone, which places on the surface a vehicle could be put down on.

1988–1997Dr Beatrix Nold
LATTICE · COM

Memory density and error correction

Not a space programme. Memory was the scarce resource in every machine the Foundation needed and the models were losing to single-bit errors at altitude. LATTICE funded the correction scheme and took no royalty on it; the grant instrument did not provide for one.

1989–1997Dr Lev Marchenko
PLUMBLINE · SUR

Surface site survey

Seventeen years of instruments flown on surface vehicles operated by others, with one job: reduce three hundred and twelve candidate sites to a shortlist a crew could be landed on. It finished with three. The Foundation then stopped surveying.

2004–2021Dr Amara Dube
WELLHEAD · SUR

Subsurface hydrogen and hydration

Neutron and passive-gamma instrumentation to find water within the first metre of regolith. Eleven candidate sites were removed from the shortlist by its first return, and the surviving sites gained a reason to be there.

2006–2019Dr Tomas Halvard
GRAVEL · SUR

Regolith mechanics

Bearing strength, trafficability, slope stability and anchor pull-out, measured in simulant and then checked against wheel-track imagery published by the operators of surface vehicles. Unglamorous, and the reason a foundation pad has a thickness.

2009–2020Dr Amara Dube
What an instrument looks like

A 1.9 kg head, built at the Aldern Works and given away

The Foundation’s first grant, in 2000, was a spectrometer bench. The flight head that came out of it was delivered to a payload integrator in 2004, crated, with a calibration certificate and a two-page manual, and returned mineralogy for six years against a design life of two.

FIG. 2 — MF/INS COMBINED SPECTROMETER HEAD, OPTICAL PATHSOURCE532 nmEXPANDERFOLDTARGET · 1.9 m STANDOFFCOLLECTORSLIT 40 µmGRATING1800 l/mmDETECTOR2048 × 256−40 °C
Fig. 2 — Combined Raman and laser-breakdown head, optical path. 532 nm source, 1.9 m standoff, 40 µm slit, 1800 l/mm grating, 2048 × 256 detector at −40 °C. Mass 1.9 kg including the radiator. Drawings and the full calibration record are in the archive.

The Foundation retains no intellectual property in this design. Three groups it has never funded have built variants of it, which is the intended outcome.

LONGBOAT · TENDER

The next five windows

Cargo precedes crew by two windows. If the 2029 uncrewed transit fails, the 2031 crew does not fly; that is written into the programme rather than left to anybody’s judgement on the day.

2027window 1
TDR-01Power plant, 1.4 MWe · 38.2 t
TDR-02Sinter works and pad plant · 31.7 t
TDR-03Consumables and spares cache · 26.4 t
2029window 2
TDR-04Habitat shell 1 · 44.1 t
TDR-05Habitat shell 2 · 44.1 t
TDR-06Water plant and stores · 29.8 t
LB-1 (U)Vessel, uncrewed shakedown transit
2031window 3
LB-1First crew of six · 258-day transit
TDR-07Habitat shell 3 and crop article · 41.6 t
2033window 4
LB-2Second crew of six · first return crew outbound relief
TDR-08Industrial plant, second phase · 36.9 t
2035window 5
LB-1Crew rotation three · continuous occupation begins
TDR-09Expansion shells 4–5 · 58.2 t

Manifests are published in full before flight. The 2027 manifest excerpt is on the history page →