CubeSTEM MissionLab Twin

M3-D Spacecraft & Subsystem Configurator · Practice only

Configuration question

Spacecraft configuration study

Change the spacecraft, preserve the environment and compare engineering evidence.

PreparingZero measured channels

Outcome

—

Baseline

—

Candidate

—

Scenario

—

Baseline spacecraft

—

Select and run a profile.

Dry mass

— kg

Battery

— Wh

Peak solar

— W

Maximum load

— W

Data rate

— kbps

Storage

— Mb

Minimum SOC

—%

Downlinked

— Mb

Overflow

— Mb

Candidate spacecraft

—

Select and run a profile.

Dry mass

— kg

Battery

— Wh

Peak solar

— W

Maximum load

— W

Data rate

— kbps

Storage

— Mb

Minimum SOC

—%

Downlinked

— Mb

Overflow

— Mb

Coupling declaration

Power, communications, payload and storage are coupled to the unchanged M3-B runtime. Mass, dimensions, inertia, center of mass and reaction-wheel values are validated and reported, but do not yet change attitude dynamics.

Comparison evidence

Run a study to generate comparison evidence.

Engineering report

A deterministic report will explain the selected profile comparison and current fidelity boundary.

Baseline: —
Candidate: —

Fidelity and authority

• Built-in profile values are explicit teaching assumptions, not CAD or flight truth.