| Project | Plan ID / revision | Test ID | Requirement / CTQ / risk IDs | Purpose / decision | Stage | Method / edition / clause | Acceptance criteria / source | Sample IDs / count / rationale | Configuration / revisions / prototype differences | Prior history / conditioning | Fixture / equipment / calibration | Operating modes / environment | Levels / units / tolerances / rationale | Sequence / duration / repetitions | Baseline / during / postchecks | Safety / stop / restart rules | Operator / lab scope | Budget / schedule | Readiness / reviewer | Actual run date | Actual results / units | Outcome / deviations | Evidence / report revision | Corrective action / retest | Result reviewer / date |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Drone Trap | TP-C1 | T01 | R01 / CTQ01 / DF01 | Verify Capture door before next gate | concept feasibility | Internal proposed method: Cycle rig then 5 N outward retention pull | Door remains latched in 100 dry capture cycles on each of 10 concept units; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Capture door and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T02 | R02 / CTQ02 / DF02 | Verify Ventilation ribs before next gate | concept feasibility | Internal proposed method: Occlude either vent bank with paper surrogate; inspect remaining airflow path | At least two independent raised vent paths remain unobstructed in bedding surrogate trial; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Ventilation ribs and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T03 | R03 / CTQ03 / DF03 | Verify Release slider before next gate | concept feasibility | Internal proposed method: Video-record unloaded representative-user task | Release grip keeps fingers 30 mm from door path; 10 adult users complete unloaded task without path contact; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Release slider and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T04 | R04 / CTQ04 / DF04 | Verify Washable shell before next gate | concept feasibility | Internal proposed method: Fluorescent soil inspection after hand wash; biological efficacy not claimed | Shell opens without tools; no visible fluorescent soil remains after defined wash on 10 units; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Washable shell and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T05 | R05 / CTQ05 / DF05 | Verify Bait pocket before next gate | concept feasibility | Internal proposed method: Force gauge pull and foreseeable misuse inspection | Bait insert remains captive after 20 N pull on 10 units; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Bait pocket and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T06 | R06 / CTQ06 / DF06 | Verify Occupancy inspection before next gate | concept feasibility | Internal proposed method: 10-user visibility/teach-back study; no live animals before ethical review | Instructions require frequent manual checks; user can see occupancy without opening; welfare reviewer sets actual interval before use; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Occupancy inspection and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T07 | R07 / CTQ07 / DF07 | Verify Entry baffle before next gate | concept feasibility | Internal proposed method: Probe each chamber loaded with surrogates in 50 cycles | Proposed 3-compartment target; rigid mouse surrogates cannot back-drive baffle at 2 N; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Entry baffle and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T08 | R08 / CTQ08 / DF08 | Verify Occupancy sensor before next gate | concept feasibility | Internal proposed method: Injected beam blockage, drift and stuck-value cases | Detect surrogate in each chamber in 100 placements including dust challenge; zero false-empty permitted in concept screen; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Occupancy sensor and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T09 | R09 / CTQ09 / DF09 | Verify Wi-Fi alert queue before next gate | concept feasibility | Internal proposed method: Router loss/reconnect and phone permission fault injection | Local occupancy indicator works without network; app marks offline within proposed 5 minutes; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Wi-Fi alert queue and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T10 | R10 / CTQ10 / DF10 | Verify BLE provisioning before next gate | concept feasibility | Internal proposed method: Threat-model-led unauthorized pairing attempts on test build | Provisioning requires physical button; unique device identity; unauthorized client denied in 50 attempts; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign BLE provisioning and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T11 | R11 / CTQ11 / DF11 | Verify Firmware updater before next gate | concept feasibility | Internal proposed method: Interrupt update at 20 points; confirm last known good boot | Local indication and mechanical capture remain safe after power interruption at each update phase; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Firmware updater and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T12 | R12 / CTQ12 / DF12 | Verify Rechargeable pack before next gate | concept feasibility | Internal proposed method: Specialist battery fault evaluation; no destructive tests by unqualified users | No charging in wet state; proposed independent overtemperature cutoff at 45 C cell surface pending battery engineer review; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Rechargeable pack and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T13 | R13 / CTQ13 / DF13 | Verify Electronics cassette before next gate | concept feasibility | Internal proposed method: Assembly interlock test and controlled splash screen; no IP rating claimed | Electronics detach before washing; power inhibited when cassette unseated; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Electronics cassette and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T14 | R14 / CTQ14 / DF14 | Verify Account and cloud before next gate | concept feasibility | Internal proposed method: Review data flows and test account deletion across backups | Collect no precise location; proposed event retention 30 days with deletion request path; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Account and cloud and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T15 | R15 / CTQ15 / DF15 | Verify Radio module integration before next gate | concept feasibility | Internal proposed method: Host pre-scan and authorization-path review; results not performed | Choose candidate module only after grant, antenna and host obligations reviewed; no FCC ID invented; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Radio module integration and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T16 | R16 / CTQ16 / DF16 | Verify Crowded chamber before next gate | concept feasibility | Internal proposed method: Surrogate occupancy/thermal analysis first; ethical live study only if approved | Capacity is not rated; proposed three isolated chambers require welfare specialist approval; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Crowded chamber and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T17 | R17 / CTQ17 / DF17 | Verify Wall-side deployment carriage before next gate | concept feasibility | Internal proposed method: Test 20 surrogate obstruction positions with power isolated emergency stop | Deployment requires clear-zone sensing and local supervised enable; obstruction forces stop before contact in unloaded trials; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Wall-side deployment carriage and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T18 | R18 / CTQ18 / DF18 | Verify Payload coupler before next gate | concept feasibility | Internal proposed method: Static 5x proposed payload proof test plus single-fault latch injection | Two independent mechanical retention paths; release impossible until ground-contact confirmation; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Payload coupler and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T19 | R19 / CTQ19 / DF19 | Verify Propeller guards before next gate | concept feasibility | Internal proposed method: Articulated probe and arm-inhibit single-fault tests | No rotor spin until guarded clearance zone verified; guarded ground fixture used first; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Propeller guards and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T20 | R20 / CTQ20 / DF20 | Verify Navigation estimator before next gate | concept feasibility | Internal proposed method: Hardware-in-loop injected 20 m position jumps and stale fixes | Containment geofence independent of mission planner; abort on estimator disagreement; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Navigation estimator and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T21 | R21 / CTQ21 / DF21 | Verify Mission battery before next gate | concept feasibility | Internal proposed method: Simulate doubled return energy and degraded pack capacity | Return energy reserve proposed at least 40% under worst-case modeled payload and wind; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Mission battery and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T22 | R22 / CTQ22 / DF22 | Verify Command link before next gate | concept feasibility | Internal proposed method: Disconnect phone, radio and cloud separately in simulation | Phone is not safety-critical; autonomous supervisor reaches predefined safe state on link loss; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Command link and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T23 | R23 / CTQ23 / DF23 | Verify Field release door before next gate | concept feasibility | Internal proposed method: Inject release command in every mission phase; verify inhibited | Release permitted only when stationary on validated landing surface with motors stopped; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Field release door and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T24 | R24 / CTQ24 / DF24 | Verify Release destination before next gate | concept feasibility | Internal proposed method: Review jurisdiction and destination documents; no destination approved | No field release until actual local species rules, landowner permission and welfare assessment recorded; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Release destination and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T25 | R25 / CTQ25 / DF25 | Verify Aircraft operation scope before next gate | concept feasibility | Internal proposed method: FAA operational applicability review including line-of-sight and authorization questions | No unattended outdoor launch; flight operations require qualified review of route, operator, airspace and permissions; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Aircraft operation scope and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T26 | R26 / CTQ26 / DF26 | Verify Remote ID equipment before next gate | concept feasibility | Internal proposed method: Bench configuration and record review; no registration asserted | Remote ID and registration applicability resolved for exact aircraft before any outdoor flight; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Remote ID equipment and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T27 | R27 / CTQ27 / DF27 | Verify Charging dock contacts before next gate | concept feasibility | Internal proposed method: Specialist fault injection of short, misalignment and sensor open | Dual isolation and independent thermal protection; no charge after failed dock alignment; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Charging dock contacts and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T28 | R28 / CTQ28 / DF28 | Verify Weather monitor before next gate | concept feasibility | Internal proposed method: Hardware-in-loop gust and missing-sensor scenarios | Research envelope proposed dry conditions and wind below 3 m/s; actual limits require flight validation; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Weather monitor and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T29 | R29 / CTQ29 / DF29 | Verify Autonomy cybersecurity before next gate | concept feasibility | Internal proposed method: Replay, tamper and privilege escalation tests in isolated rig | Only authenticated signed mission plan; user cannot bypass safety envelope remotely; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Autonomy cybersecurity and repeat linked tests | Not reviewed |
| Drone Trap | TP-C1 | T30 | R30 / CTQ30 / DF30 | Verify Return docking before next gate | concept feasibility | Internal proposed method: Simulate moved dock, marker occlusion and blocked return path | Maximum one failed docking attempt then designated safe land; no repeated wall approach; scenario C1 not approved | 10 mechanical prototypes or one simulated system across listed fault cases; screening sample, not certification | Drone Trap C1; prototype uses surrogates and isolated rigs; no released hardware | Baseline clean/dry; repeat dirty/worn condition where relevant | Force gauge/temperature logger/video or HIL harness; calibration before use | Indoor controlled bench; flight simulation only; representative misuse injected | Criterion above is proposed; numerical limits require qualified engineering/welfare review | Per described method; log every cycle/fault and state transition | Baseline function; monitor safety states; final containment/visual check | Stop on distress surrogate failure, unexpected motion, heat or interlock defeat; specialist authorizes restart | Jordan Vale; independent specialist for hazardous tests | Included in $250000 feasibility allowance; internal target 2027-06-15 | Not ready — design/safety review first | Not run | No actual results | Not run; no pass or deviation claimed | No report exists | If fail: redesign Return docking and repeat linked tests | Not reviewed |
Sample — fictitious company. All numbers and people are invented scenario assumptions. This is draft concept paperwork; no physical testing, customer evidence, certification, filing or sign-off has occurred.