Design a mechanism gear mesh against ECSS-E-ST-33-01C clause 4.7.5.4.7. Use when a spur or helical stage must be shown good for tooth strength, flank wear, backlash and life together: forming the tangential tooth force from module and torque, computing the Lewis bending stress and the Hertzian flank contact stress, derating both material allowables for the required tooth load cycles, sweeping backlash across the thermal range for the gear-to-housing expansion mismatch, and checking the lubric...
Scanned 9/27/2026
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---
name: e3301-gear-design
description: "Design a mechanism gear mesh against ECSS-E-ST-33-01C clause 4.7.5.4.7. Use when a spur or helical stage must be shown good for tooth strength, flank wear, backlash and life together: forming the tangential tooth force from module and torque, computing the Lewis bending stress and the Hertzian flank contact stress, derating both material allowables for the required tooth load cycles, sweeping backlash across the thermal range for the gear-to-housing expansion mismatch, and checking the lubricant against that range, the flank stress and the gear material. Trigger: ecss, e-st-33-01-mechanisms-scope, gear-tooth-bending-stress, gear-flank-contact-stress, gear-backlash-thermal-range, gear-lubricant-compatibility, gear-tooth-load-cycles, lewis-form-factor."
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-33-01-mechanisms-scope, e3301-gear-design, gear-tooth-bending-stress, gear-flank-contact-stress, gear-backlash-thermal-range, gear-lubricant-compatibility, gear-tooth-load-cycles, lewis-form-factor]
version: 0.1.0
author: Aero Agent Skills
---
# ECSS Mechanisms — Gear Design (space-systems/ecss/e3301-gear-design)
Use when the task is the gear design of ECSS-E-ST-33-01C clause
4.7.5.4.7 -- showing that a mesh inside a space mechanism carries its
torque without breaking a tooth or pitting a flank, keeps a positive
and bounded backlash over the whole thermal range, sits in a lubricant
it is compatible with, and does all of that for the required number of
tooth load cycles.
## Domain quick reference
- A gear mesh has two independent strength checks, not one. Tooth
bending is a root-fillet stress that scales linearly with tooth force;
flank durability is a Hertzian contact stress that scales with the
square root of it. A change that fixes one -- a finer module, a wider
face, a different material -- moves the other by a different amount,
so both are recomputed after every change.
- The Lewis form factor is a function of tooth count, and it falls
sharply below about twenty teeth. A pinion chosen small to fit a
packaging envelope pays for it twice: fewer teeth carry the same
torque at a smaller pitch diameter, and each of those teeth is
intrinsically weaker in bending.
- Flank contact stress carries the elastic coefficient of the material
pair. A steel pinion running on a polymer wheel is a far softer
contact than steel on steel, which lowers the stress and lowers the
allowable much further; the pairing is assessed as a pair.
- Allowables are quoted at a reference life. Above it they are derated
on a Woehler slope; below it no credit is taken, because a short-life
mechanism does not get a stronger material.
- Backlash is a thermal quantity. The centre distance moves with the
difference between the gear expansion and the housing expansion, and
that motion appears at the mesh multiplied by twice the tangent of the
pressure angle. A steel mesh in an aluminium housing loses backlash
cold and gains it hot, so both extremes are checked against a floor
above zero and a bound above the nominal.
- Lubricant selection is three checks at once: the qualification
temperature range against the lubricant rating, the flank contact
stress against the load the film is credited to, and the gear material
against what the lubricant may sit on. A dry film that needs a
metallic substrate and a grease that degrades on fresh steel under
boundary conditions both fail on the third check, not the first.
## Workflow
1. Validate the mesh: module, pinion and wheel tooth counts, face width
and transmitted torque, and both materials. A tooth count below the
tabulated form-factor range is an input error, not a value to
extrapolate.
2. Derive the pitch diameters, the centre distance and the tangential
tooth force at the pinion pitch circle.
3. Compute the Lewis bending stress with the form factor of the pinion
tooth count and the dynamic factor of the drive.
4. Compute the elastic coefficient of the material pair and from it the
flank contact stress at the same tooth force.
5. Derate both allowables for the required tooth load cycles and compare
each stress against its derated allowable, absorbing representation
error at the boundary with a named tolerance.
6. Sweep the backlash across the cold case, the assembly temperature and
the hot case; hold the minimum above the floor and, when a bound is
specified, the maximum below it.
7. Run the lubricant against the temperature range, the computed flank
stress and the gear material, and return every finding with the
numbers that produced it.
## Pitfalls
- Sizing on bending alone. A tooth that passes Lewis comfortably can
still pit its flank within the mission cycle count, and pitting is the
failure mode that shows up in a life test rather than a proof load.
- Taking the backlash measured at assembly as the backlash in orbit. The
number that matters is the cold-case minimum with the housing
expansion mismatch applied, and it can be a large fraction of the
assembled value.
- Checking the cold case only. An oversized hot-case backlash costs
pointing accuracy and can let the mesh rattle through a launch
vibration case, so the upper bound is a requirement too.
- Applying the life derating below the reference life. It is a knockdown
above the reference, never a credit below it; a short-life mechanism
keeps the tabulated allowable and no more.
- Choosing a lubricant on temperature range alone. The contact stress
the film is credited to, and the substrate the film needs, fail
independently of temperature and are the checks most often skipped.
- Reusing a qualified mesh at a higher torque because the stresses still
look comfortable. Both allowables depend on the cycle count, so a
duty-cycle change re-opens the strength case even when the geometry is
untouched.
## Behavior contract (gate 3)
The mesh validation, tangential force, Lewis form factor and bending
stress, elastic coefficient and flank contact stress, life derating,
thermal backlash sweep and lubricant compatibility screen are exercised
by the gate 3 contract test: scripts/test_e3301_gear_design.py against
scripts/e3301_gear_design_logic.py (stdlib unittest, offline). Run:
python3 scripts/test_e3301_gear_design.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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