VECTORIS LUNA

Research programs

Five domains inside LUNA. A planned program is still a public research question. No program is a completed habitat design.

VL-PROG-HABACTIVE

Lunar Habitat Structures

How can pressure-shell, buckling and buried-shell screening be made traceable enough to support later design-level structural workflows?

  • Classical thin/thick pressure-shell relations are implemented as screening kernels.
  • Preliminary classical buckling screening exists; knockdown and imperfection sensitivity are not closed.
  • No qualified habitat design method is claimed.

Models: VL-MOD-PSH-001 · VL-MOD-PSH-002 · VL-MOD-BCK-001 · VL-MOD-BRI-001

Gaps: VL-GAP-006 · VL-GAP-007

Implementation: Pressure-shell kernels implemented; buckling and buried-shell interaction remain screening-level.

Validation: Screening only. Planned analytical comparisons are recorded in VL-BENCH-001 and have not been run.

VL-PROG-REGACTIVE

Regolith Geotechnics

Which continuum screening models for density, overburden and lateral pressure can be justified before site-specific and low-gravity constitutive data exist?

  • A density-depth working model and overburden integration are implemented.
  • K0 / Rankine screening is used as a bound, not as unique physical truth.
  • South Pole stratigraphy, ice content and low-gravity constitutive behaviour remain open.

Models: VL-MOD-REG-001 · VL-MOD-REG-002 · VL-MOD-GEO-001 · VL-MOD-BRI-001

Gaps: VL-GAP-001 · VL-GAP-002 · VL-GAP-003 · VL-GAP-006

Implementation: Density-depth, overburden and Rankine/K0 screening kernels are implemented.

Validation: Screening only. No site-specific geotechnical validation is claimed.

VL-PROG-ISRUPLANNED

Lunar Construction Materials / ISRU

What evidence is required before sintered or process-route regolith products can be treated as structural materials rather than research concepts?

  • No Vectoris structural allowable set exists for ISRU products.
  • VL-SRC-001 records community practice on simulants and sintering as context only.
  • Qualification of ISRU materials is an open gap.

Models: none implemented

Gaps: VL-GAP-004

Implementation: No ISRU constitutive or allowable kernel is implemented.

Validation: Not started as a materials qualification program.

VL-PROG-THMACTIVE

Lunar Thermal & Environmental Engineering

How should vacuum, thermal cycling and environmental loads be introduced into structural screening without implying a qualified thermal-control design?

  • A lunar gravity / environment baseline is implemented for screening.
  • Preliminary thermal and transient wall models exist at screening status.
  • Integrated thermal-structural validation is not closed.

Models: VL-MOD-ENV-001 · VL-MOD-THM-001 · VL-MOD-THM-002

Gaps: VL-GAP-009

Implementation: Environment baseline implemented; thermal kernels remain screening-level.

Validation: Screening only. Coupled thermal-structural benchmarks are not published.

VL-PROG-SURPLANNED

Lunar Surface Infrastructure

Which surface-system loads (plume, ejecta, MMOD, landing proximity) can enter a structural workflow only after dedicated models and evidence exist?

  • No LUNA plume, MMOD or landing-load kernel is implemented.
  • These topics are recorded as open model and data gaps.

Models: none implemented

Gaps: VL-GAP-007 · VL-GAP-008

Implementation: No surface-infrastructure load kernels implemented.

Validation: Not started.