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instrument / verified-clean
Optimal Launch Angle Finder
The current ledger marks this instrument verified clean within the source-bound verification corpus.
Inspectable records
Ledger state
The current ledger marks this instrument verified clean within the source-bound verification corpus.
- Area
- Physics
- Tranche
- tranche-2
- Evidence ID
- t2-023
- Ledger rows
- 1
No ledger note is attached.
Review findings
The supplied maximum-range angle formula is valid only for the stated vacuum maximum-range problem, not for the broader target-hitting claim. The instrument should either remove target-solving claims or add the projectile trajectory and target-angle equations, feasibility checks, and the complete range formula.
Formula and scope findings
- The level-ground optimum θ_max=45° is correct only for a vacuum projectile with equal launch and landing elevations, positive launch speed, and uniform positive gravitational acceleration.
- The height-offset formula θ=atan(v0/√(v0²+2gh0)) is correct for maximizing horizontal range when h0 is the launch height above the landing level, with v0>0, g>0, and h0≥0. These domain constraints are not stated.
- The specification claims the instrument can find an angle that hits a target, but no target-trajectory equation or target-angle solution is provided. Hitting a target generally yields zero, one, or two feasible angles depending on distance, height, speed, and constraints.
- The specification claims to output resulting range, but no range formula is provided. The required vacuum-model range formula is R=(v0 cosθ/g)(v0 sinθ+√(v0²sin²θ+2gh0)); at the maximizing angle for h0≥0 this simplifies to R_max=(v0/g)√(v0²+2gh0).
- The formula does not define behavior for h0<0, v0=0, g≤0, or v0²+2gh0≤0.
Unit assumptions
- Use a consistent unit system: v0 in m/s, g in m/s², h0 and range in m, and angles in degrees for display.
- The example with v0=72 km/h requires conversion to 20 m/s before applying the formula.
- g is uniform gravitational acceleration and is normally 9.81 m/s² near Earth.
- atan returns an angle in radians internally; convert to degrees for the displayed angle.
- h0 means launch height above the landing level, not an arbitrary signed height offset.
Boundary hardening
BREAK_CLAIMED · SELF_FLAGGED
The height h0=-v0^2/(2g) makes sqrt(v0^2+2gh0)=0, so the angle formula divides by zero and the expected result is undefined. The instrument should reject this input.
Errata and corrections
No applied erratum is attached to this unique-name record.
Inspectable example
4 review vectors are recorded. One source-bound sample is shown below.
{
"inputs": {
"v0": 20,
"g": 9.81,
"h0": 0,
"units": "SI"
},
"expected_outputs": {
"optimal_angle_deg": 45,
"resulting_range_m": 40.7747
},
"working": "θ=atan(20/√(20²+2×9.81×0))=atan(20/20)=atan(1)=45°. R_max=(20/9.81)×√(20²+0)=(20/9.81)×20=400/9.81=40.7747 m."
}Related workflows
Sources and evidence
These pointers bind the page to evidence. They do not grant authority or collapse verification into deployment.
VERIFIED_LEDGER.json · VERIFIED_CLEANevidence-tranche2/tranche2-results.jsonBOUNDARY_HAZARD_CATALOG.json