geoprimsField-grade geospatial math

Drone impact kinetic energy

Kinetic energy ½mv² in joules and foot-pounds, compared with the 80 J threshold and the category 2 operations-over-people 11 ft-lb threshold, each cited.

Planning and education aid. Not for primary navigation. Full disclaimer

Experimental: not yet fully verified. How results are checked

162.5J

At that speed it carries 162.5 J (119.8 ft*lbf). Not legal advice.

Kinetic energy
EASA class C1
FAA operations over people, category 2
Notice
Provenance
Computed by
drone.ops.kinetic-energy 1.0.0, core 0.1.0
Model
KE = ½·m·v²; C1 needs MTOM under 900 g or under 80 J transferred in a head-on impact at terminal velocity; category 2 is set by 11 ft-lb of transferred energy
Accuracy
Exact kinetic energy. Both regulations judge transferred energy under a test method, so this is a screening value, not a compliance finding.
Notes
1 shown with the answer
Cites
European Commission, Commission Delegated Regulation (EU) 2019/945 on unmanned aircraft systems and third-country operators; Federal Aviation Administration, 14 CFR Part 107, Small Unmanned Aircraft Systems

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How we got thisFormula, worked example, sources, and proof

Model: KE = ½·m·v²; C1 needs MTOM under 900 g or under 80 J transferred in a head-on impact at terminal velocity; category 2 is set by 11 ft-lb of transferred energy

Accuracy: Exact kinetic energy. Both regulations judge transferred energy under a test method, so this is a screening value, not a compliance finding.

Worked example: A 0.9 kg drone at 19 m/s. Source: add-drone-suite C1 scenario: 162.5 J, above 80 J. It is golden test vector v001, and every build checks the tool still gives its answer within its tolerance.

You enter

Mass
0.9 kg
Speed
19 m/s

You get

Kinetic energy
162.5 J
Kinetic energy
119.8 ft*lbf
EASA class C1
162.5 J exceeds 80 J and the mass is 900 g or more, so this drone cannot meet C1, which needs under 900 g or under 80 J (Regulation (EU) 2019/945, Annex Part 2 (class C1)).
FAA operations over people, category 2
119.8 ft*lbf is above the 11 ft-lb category 2 threshold (14 CFR 107.120(a)(1)), which applies to energy transferred on impact, shown by an accepted means of compliance.
Notice
Summary of rules as of 2026-09-18. Not legal advice. Check the current regulation and any waivers, authorizations, or local restrictions: https://eur-lex.europa.eu/eli/reg_del/2019/945/oj

Review: Not yet independently reviewed by a Part 107 remote pilot.

Last verified: 2026-09-18, when a maintainer last confirmed this tool's sources at the issuer. See the sources ledger.

Status: version 1.0.0, core 0.1.0. See this tool in the verification report.

Checked against: 5 golden test vectors (download the test vectors, each with its source and tolerance). See how results are checked and every source.

Sources

Terms

C1: EASA class C1
An EASA drone class: under 900 g, or under 80 J of impact energy, meant for the A1 open subcategory. Source: Regulation (EU) 2019/945
EASA: European Union Aviation Safety Agency
The EU agency that sets aviation safety rules, including the drone rules in Regulations (EU) 2019/947 and 2019/945. Source: EASA Guidelines for UAS operations in the open and specific category
FAA: Federal Aviation Administration
The US civil aviation authority. Source: 14 CFR Part 1 definitions

Experimental means this tool has not yet met the stable bar: at least 20 golden vectors, differential tests, and an independent worked example.

C1 — EASA class C1

An EASA drone class: under 900 g, or under 80 J of impact energy, meant for the A1 open subcategory.

Source: Regulation (EU) 2019/945

EASA — European Union Aviation Safety Agency

The EU agency that sets aviation safety rules, including the drone rules in Regulations (EU) 2019/947 and 2019/945.

Source: EASA Guidelines for UAS operations in the open and specific category

FAA — Federal Aviation Administration

The US civil aviation authority.

Source: 14 CFR Part 1 definitions