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APEX TECHNICAL

FDB-0025 · ORIGINAL SOURCE VALUE

ASM-G-B7-000002

Registry: engineering_assumption_registry. Original field names and values are displayed without translation or reinterpretation.

applicability_boundary
Engineering prediction for the declared Aerrow/FC002/T700/16 mm PP honeycomb/semi-hot-press working configuration under stated assumptions. The declared configuration is not proof of as-built material identity, lot identity, laminate architecture, bondline, or actual physical performance.
assumption_id
ASM-G-B7-000002
assumption_lower
14.5
assumption_nominal
15
assumption_upper
15.3
data_class
ASSUMPTION
description
Effective core thickness is bounded after subtracting two assumed face sheets from the declared 16 mm total thickness.
reason_required
As-built core and face thicknesses are unavailable.
sensitivity_level
HIGH
supporting_reference_ids
REF-G-B7-000027
test_action_ids
TESTACT-G-B4-000020|TESTACT-G-B4-000013|TESTACT-G-B4-000022
uncertainty_contribution
Directly affects areal mass, shear area and sandwich lever arm.
units
mm

Identifiers mentioned in source fields

These are search links, not inferred engineering relationships.

Provenance

archiveSha256
ded5d3a55705d2387a6fec03fd5fd9c93d948acca3c3de8c66ed7a82fca45cc5
virtual_path
!/PICKLEBALL_DATABASE_APPROVED_FROZEN_BASELINES_THROUGH_STAGEG_CROSS_TEST_CORRELATION_AND_PADDLE_ENGINEERING_PROFILE_REV1_2026-09-15.zip!/frozen_history/PICKLEBALL_DATABASE_APPROVED_FROZEN_BASELINES_THROUGH_STAGEG_FIRST_ENGINEERING_PREDICTIVE_VALIDATION_REV1_2026-09-15.zip!/stage_g_b7_first_engineering_predictive_validation/approved_payload/STAGEG_B7_FIRST_ENGINEERING_PREDICTIVE_VALIDATION_BASELINE_REV1_2026-09-14.zip!/STAGEG_B7_FIRST_ENGINEERING_PREDICTIVE_VALIDATION_BASELINE_REV1/engineering_assumption_registry.csv
source_file_sha256
1073c4d58d4916b3555425b7b549c24bc141e61f5a2ea1156a7774fe0944f6b0
source_locator
csv:row:2
fields_sha256
ed74337d344b360a515f1ab111cbc6f6e47a56495f357add28a6d93cfaf13410
source_version
FDB-0025