Documented limits, not marketing promises

Operating Philosophy

Documented limits, not marketing promises

We treat every platform as a systems-integration problem, and we publish the reasoning before the render. Mobility, positioning, power, thermal budget, dust tolerance, avionics interfaces, and redundancy are stated with margins and boundaries attached. Here is what is qualified, and here is what is not. Moon Buggies is a fictional design studio; we claim no flight or test heritage. Every performance figure carries a unit and a documented margin, so you can self-qualify your mission profile before you contact us.

Review qualification posture

Qualification status

What is qualified, and what is not yet

Qualified

In progress

Not yet qualified

Capability

Status

Documented boundary

Mobility & suspension over graded regolith slopes

Qualified — analysis only

20° grade with 15% traction margin in the illustrative nominal case.

GNSS-denied surface positioning

In progress — budget open

Dead-reckoning plus terrain-relative navigation architecture is fixed. Documented position error budget is not yet closed; long-traverse drift remains unbounded pending analysis. Do not assume mission-grade absolute accuracy.

Thermal management across the lunar day/night cycle

Qualified — steady-state analysis

Not yet qualified for extended permanently-shadowed-region dwell without supplemental heat rejection.

Dust tolerance and regolith abrasion resistance

In progress — material selection under review

Seal and bearing concepts selected for abrasive ingress resistance. Cycle-life under repeated regolith exposure is not yet characterized. Treat abrasion durability as an open item, not a stated limit.

Avionics interface and redundancy architecture

Qualified — interface definitions documented

Mechanical, electrical, thermal, and data interfaces are documented as ICD drafts with dual-string redundancy on critical paths. Fault-tolerance testing is not yet performed. Interface boundaries are firm; verification evidence is pending.

Crewed egress and human-rated operations

Not yet qualified

No crew-safety analysis, egress path validation, or human-rating posture exists. Not offered for crewed operations. Any crewed mission profile requires a separate, from-scratch qualification program.

Mobility & suspension over graded regolith slopes

Qualified — analysis only

20° grade with 15% traction margin in the illustrative nominal case.

GNSS-denied surface positioning

In progress — budget open

Dead-reckoning plus terrain-relative navigation architecture is fixed. Documented position error budget is not yet closed; long-traverse drift remains unbounded pending analysis. Do not assume mission-grade absolute accuracy.

Thermal management across the lunar day/night cycle

Qualified — steady-state analysis

Not yet qualified for extended permanently-shadowed-region dwell without supplemental heat rejection.

Dust tolerance and regolith abrasion resistance

In progress — material selection under review

Seal and bearing concepts selected for abrasive ingress resistance. Cycle-life under repeated regolith exposure is not yet characterized. Treat abrasion durability as an open item, not a stated limit.

Avionics interface and redundancy architecture

Qualified — interface definitions documented

Mechanical, electrical, thermal, and data interfaces are documented as ICD drafts with dual-string redundancy on critical paths. Fault-tolerance testing is not yet performed. Interface boundaries are firm; verification evidence is pending.

Crewed egress and human-rated operations

Not yet qualified

No crew-safety analysis, egress path validation, or human-rating posture exists. Not offered for crewed operations. Any crewed mission profile requires a separate, from-scratch qualification program.

Evidence before render

The margin table comes before the render

We publish the qualification matrix, operational-limit tables, and documented margins first. The exploded diagram and any visual comes second, annotated with the same numbers. Each claim carries a value, a unit, and a margin — or it is marked not yet qualified. This is a fictional-project studio; no flight or test heritage is implied. What you read is the reasoning, stated as it would stand in a design review.

Trust Posture

Qualification stated as posture, not heritage

Moon Buggies is a fictional design studio with no claimed flight or test heritage. Its systems are documented against analysis and stated assumptions, not mission history. The matrix separates qualified analysis, work in progress, and open boundaries. Each margin names its unit and study case; absent evidence stays visibly absent.

Read the matrix, then open the conversation

Bring your thermal budget, positioning constraints, and interface definitions. We will compare them with the study limits and state where the fit holds—and where it does not.

Start Mission-Fit Review