Use when ground support equipment (GSE) will interface with flight hardware during verification and needs to be qualified as verification tooling before use, consistent with ECSS-E-ST-10-02C clause 5.2.6.2 (GSE qualification) and the general tool-qualification regime of clause 5.2.6.1. Classifies GSE as mechanical (MGSE) or electrical (EGSE) and determines the required qualification actions (interface control document, proof test, periodic re-proof, interface safety verification, calibration ...
Scanned 9/27/2026
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---
name: e1002-gse-tools
description: "Use when ground support equipment (GSE) will interface with flight hardware during verification and needs to be qualified as verification tooling before use, consistent with ECSS-E-ST-10-02C clause 5.2.6.2 (GSE qualification) and the general tool-qualification regime of clause 5.2.6.1. Classifies GSE as mechanical (MGSE) or electrical (EGSE) and determines the required qualification actions (interface control document, proof test, periodic re-proof, interface safety verification, calibration with traceability). Trigger: GSE, ground support equipment, MGSE, EGSE, proof test, handling equipment, test stimulation equipment, tool qualification, E-ST-10-02, verification tooling, ecss, e-st-10c."
license: Apache-2.0
compliance: STANDARDS-REF
standards:
- id: ecss
reference-only: true
gated: false
domain: space-systems
pack: space-systems
compatibility: "agentskills.io SKILL.md; any SKILL.md host (Claude Code, Hermes, OpenClaw)"
metadata:
domain: space-systems
subdomain: ecss
tags: [ecss, e-st-10c, gse, mgse, egse, verification-tooling, tool-qualification]
version: 0.1.0
author: Aero Agent Skills
---
# ECSS GSE Qualification for Verification Tooling (space-systems/ecss/e1002-gse-tools)
Use when the task is qualifying ground support equipment (GSE) that
will be used as verification tooling under ECSS-E-ST-10-02C, ahead of
letting that GSE contact, handle, stimulate, or measure flight
hardware.
## Domain quick reference
- ECSS-E-ST-10-02C clause 5.2.6.2 requires GSE used in verification to
itself be qualified before it interfaces with flight hardware,
extending the general tool-qualification regime of clause 5.2.6.1
(see the sibling e1002-tools-general leaf).
- GSE splits into two classes: MGSE (mechanical GSE -- handling,
lifting, transport, alignment fixtures, protective covers) and EGSE
(electrical GSE -- test stimulation, simulation, power supplies,
signal/checkout equipment, harnesses).
- MGSE that physically contacts the flight item carries a structural
risk and needs a proof test (loaded above design load) before first
use, plus periodic re-proof (after modification, or once usage since
the last proof reaches the item's allowed limit).
- EGSE that electrically interfaces the flight item carries an
over-stress risk and needs an interface safety verification
confirming it cannot deliver an out-of-spec stimulus to the flight
item.
- Any GSE acting as the measurement or stimulus of record for a formal
verification result -- of either class -- needs calibration with
traceability, because its accuracy directly bounds the verification
result's credibility.
- Any GSE that contacts or interfaces the flight item, of either
class, needs an interface control document (ICD) so that GSE
configuration changes are tracked like a flight interface change.
## Workflow
1. For each GSE item used in the verification programme, record its
primary function, whether it contacts or otherwise interfaces the
flight item, and whether it is the measurement or stimulus of
record for a formal verification result.
2. Classify the GSE as MGSE or EGSE from its primary function.
3. Derive the required qualification actions for the item: ICD if it
interfaces the flight item; proof test and periodic re-proof if it
is MGSE that contacts the flight item; interface safety
verification if it is EGSE that interfaces the flight item;
calibration with traceability if it is the measurement/stimulus of
record.
4. Build the GSE register: one classification and required-action set
per GSE id, and confirm no GSE id used in the verification
programme is missing from the register.
5. Before releasing any GSE item for use with flight hardware, check
its required actions against the actions actually completed and
block use on any gap; treat an item with no completion record as
fully unqualified rather than assuming it is covered.
6. For MGSE items requiring periodic re-proof, track modification and
usage-since-last-proof and flag any item due for re-proof (or with
no re-proof status on record) before its next use.
7. Hand the register and any measurement-chain GSE ids to the
Verification Plan tooling section (E-ST-10-02 clause 5.2.8.1) and
to the general tool-qualification record (e1002-tools-general).
## Pitfalls
- Letting MGSE contact flight hardware without a proof test, or
treating an old proof test as still valid after a modification.
- Treating EGSE as risk-free because it does not touch the flight item
mechanically, and skipping the interface safety verification for a
stimulus or power interface.
- Missing that GSE serving as the sensor of record for a verification
measurement needs its own calibration and traceability, even when
its class would not otherwise require special qualification.
- Assuming a GSE item with no completion or re-proof record is fine to
use, instead of treating the missing record as a qualification gap.
## Behavior contract (gate 3)
The classification, required-action, register-completeness, and
re-proof-due logic is exercised by the gate 3 contract test:
scripts/test_e1002_gse_tools.py against
scripts/e1002_gse_tools_logic.py (stdlib unittest, offline). Run:
python3 scripts/test_e1002_gse_tools.py
## Compliance
- ECSS standards are freely downloadable (ESA); cite the source and
paraphrase per standards-map.yaml.
- compliance: STANDARDS-REF, gated: false.
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