The Standards Map — Humanoid Robotics Pack Qualification, Q3 2026 Update
Four adjacent-framework documents updated this quarter. UL 2595 Ed 3 raised its voltage ceiling from 75 Vdc to 250 Vdc, which brings most humanoid pack architectures inside its stated scope for the first time. ISO 18646-5:2026 standardizes legged-robot locomotion test methods and contains no battery parameter, though it supplies useful structure for anchoring duty-cycle definition. UL 3300 revised whole-machine moisture and stability clauses. UN 38.3 Rev 8 Am 1 is a citation update. None of it closes the pack-qualification gap: every DVP row in the gaps table remains program-defined, and ISO 13482 Edition 2 has been at FDIS since July 2025.
The Standards Map — Humanoid Robotics Pack Qualification, Q3 2026 Update
Four adjacent-framework documents updated this quarter. UL 2595 Ed 3 raised its voltage ceiling from 75 Vdc to 250 Vdc, which brings most humanoid pack architectures inside its stated scope for the first time. ISO 18646-5:2026 standardizes legged-robot locomotion test methods and contains no battery parameter, though it supplies useful structure for anchoring duty-cycle definition. UL 3300 revised whole-machine moisture and stability clauses. UN 38.3 Rev 8 Am 1 is a citation update. None of it closes the pack-qualification gap: every DVP row in the gaps table remains program-defined, and ISO 13482 Edition 2 has been at FDIS since July 2025.
Gap Context Research
Battery Thermal Runaway in eVTOL Aircraft: Risks, Mitigations, and Firefighting Strategies (CAP3203)
DO-311A was not developed for propulsion-scale batteries. CAP3203 documents the scope limitation explicitly, confirming the multi-document regulatory posture EASA MOC guidance attempts to address.
Post-crash and external-fire scenarios lack standards-body activity and eVTOL-specific empirical data. Pack-level emergency response test criteria remain program-defined.
Gap Context Research
Powering Humanoid Robots: The Central Role of Battery Technology
None exists. The authors state the gap directly. Every pack-level parameter in this paper is Tier 3 sourced from engineering analysis, not from a published standard.
Acceptance criteria for humanoid pack qualification must be program-defined and defensibly documented. Adjacent-domain borrowing (ISO 13482, IEC 62619) requires explicit justification per parameter.
Light-Sport Lane Primer
14 CFR Part 22, effective July 24, 2026 under the MOSAIC final rule, created a light-sport powered-lift category that operates on manufacturer self-certification. The FAA issues no type certificate and conducts no bilateral MOC negotiation. The manufacturer signs a statement of compliance (FAA Form 8130-15) attesting conformance with FAA-accepted ASTM consensus standards.
The battery qualification standard in this lane is ASTM F3830-26, Electrical Energy Storage Systems, published June 2026, covering design, installation, and qualification of rechargeable lithium propulsion EESS. The FAA's powered-lift MOC table maps F3830-26 to five Subpart B requirements: §22.125, §22.130, §22.135, §22.145, and §22.155.
The accepting-authority structure is what matters for DVP work. F3830-26 does not satisfy a showing under AC 21.17-4. DO-311A and EASA MOC-3 do not satisfy a Part 22 SOC. These are different regulatory instruments accepted by different authorities, and citing across them is unresponsive to the lane you are actually qualifying in. F3830-26 is four pages and paywalled; at that length it almost certainly delegates test parameters to referenced standards, which means clause-level thresholds require chasing those references before any value enters a DVP.
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