Battery Drop-Readiness for an Advanced Air Mobility Platform
Aerospace & Electrified Aviation

Context
Early-to-mid-stage battery enclosure design for an electrified aircraft program with strict safety milestones.
Challenge
The team needed to reduce crash/drop validation risk while design and supplier constraints were still changing.
Approach
Built a structured simulation matrix for drop, impact, and maneuver-related load paths, then used iterative model reviews to prioritize design updates and test focus areas.
Outcome
Improved validation readiness and reduced redesign loops through earlier risk visibility and clearer decision sequencing.
Deliverables
- Model package with assumptions register
- Load-case matrix linked to program decisions
- Design recommendation brief with risk ranking
- Validation planning memo for upcoming tests
Standards Context
MC-VTOL | DO-160G-aligned workflows | UN transport-safety context
Details generalized to protect confidential client programs.

