Model how payload, altitude, and battery life influence the ground area each aerial seeding flight can treat.
This calculator estimates how much ground a drone can cover per flight during aerial seeding missions and how many flights you will need to hit your reforestation target. It is designed for conservation teams, NGOs, startups, and landowners who are experimenting with drone-based reforestation or landscape restoration.
By entering your target area, desired seed density, drone payload capacity, release altitude, seed spread angle, flight speed, and battery life, the planner estimates:
This is a mission-planning tool rather than a full ecological model. It helps you translate drone and payload specifications into operational coverage, so you can compare hardware options, plan crew schedules, and spot obvious constraints before field deployment.
The calculator uses the metric system: distances in meters, areas in hectares (1 hectare = 10,000 m²), and seed density in seeds per square meter. Keeping units consistent is important for meaningful results.
The tool uses a simplified geometric and kinematic model to approximate coverage. It assumes that seeds disperse in a conical pattern underneath the drone and that the drone flies in straight, level passes over the area of interest.
The seed spread is approximated as a cone with spread angle θ (in degrees) and release altitude h (in meters). The effective swath width w on the ground is:
where:
A larger spread angle or higher altitude increases the swath width, but in practice also increases exposure to wind drift and uneven distribution.
Flight distance is based on horizontal speed and battery life. Let:
Convert battery life to seconds: ts = 60 × t. The maximum straight-line distance the drone could fly while seeding is:
df = v × ts
Assuming continuous seeding over this distance and swath width w, the battery-limited coverage area is:
Ab = df × w (in m²)
Payload limits how many seeds can be released in a flight. Let:
If you aim for a uniform density ρs, the maximum area you can seed before running out of seeds is:
Ap = Ns / ρs (in m²)
This reflects the ecological target: higher desired density (more seeds per square meter) reduces payload-limited coverage per flight.
The true coverage per flight is limited by whichever factor runs out first: battery or payload. The calculator takes the minimum of the two areas:
Ac = min(Ab, Ap)
Let your total target area be At. You enter this in hectares, so the planner converts it internally:
At,m² = At,ha × 10,000
The number of sorties (flights) needed is then:
sorties = ceil(At,m² / Ac)
where ceil means “round up to the next whole number,” because you cannot fly a fraction of a mission.
Consider a team reseeding land after a wildfire. Their mission parameters are:
Using h = 50 m and θ = 60°:
w = 2 × 50 × tan(60° / 2) = 100 × tan(30°) ≈ 100 × 0.5774 ≈ 57.74 m
Battery life in seconds: ts = 15 × 60 = 900 s.
Flight distance: df = 10 m/s × 900 s = 9,000 m.
Battery-limited coverage area:
Ab = df × w ≈ 9,000 × 57.74 ≈ 519,660 m²
In hectares, this would be roughly 51.97 ha if payload were unlimited.
Payload capacity: Ns = 10,000 seed balls.
Desired density: ρs = 3 seeds/m².
Payload-limited coverage area:
Ap = Ns / ρs = 10,000 / 3 ≈ 3,333 m²
This equals 0.333 hectares per flight.
The actual coverage per flight is the minimum of 519,660 m² and 3,333 m², which is 3,333 m². The team is clearly payload-limited, not battery-limited.
Target area in square meters: At,m² = 15 × 10,000 = 150,000 m².
Number of flights needed:
sorties = ceil(150,000 / 3,333) ≈ ceil(45) = 45
Each flight uses roughly 15 minutes of battery life, so total time in the air is about 675 minutes, or 11.25 hours. Real missions will also include time for takeoff, landing, battery swaps, loading seeds, and transit, so field time will be longer.
Changing payload and battery capacity affects coverage differently depending on which constraint dominates. The table below shows simplified scenarios based on the example above, holding all other parameters constant.
| Scenario | Payload (seeds) | Battery (min) | Area per flight (ha) | Primary constraint |
|---|---|---|---|---|
| Baseline | 10,000 | 15 | 0.333 | Payload-limited |
| Larger hopper | 20,000 | 15 | 0.667 | Payload-limited |
| Longer battery | 10,000 | 30 | 0.333 | Payload-limited |
| Balanced upgrade | 20,000 | 30 | ≈1.33 (until battery becomes limiting) | Mixed, shifting toward battery |
When you are payload-limited, doubling payload nearly doubles coverage per flight and halves the required number of sorties. Doubling battery life alone does not help until payload and other factors are sufficient for battery to become the limiting factor. Use the planner to explore several configurations and identify the most impactful upgrades for your operations.
After you enter your inputs and run the calculation, you will typically see:
Use these values for high-level mission planning:
Remember that the calculator estimates ground coverage, not germination rates or long-term forest establishment. For ecological success, you must also consider species selection, soil preparation, and post-planting monitoring.
This planner is intentionally simplified. When using its outputs, keep these key assumptions and limitations in mind:
Because of these limitations, treat the planner as a strategic planning and comparison tool. Validate key parameters with small test flights and ground truthing before committing to large-scale deployments.
For responsible reforestation, combine this calculator with local ecological expertise and on-the-ground data. Before a mission, consult forestry agencies, landowners, and relevant authorities; verify that selected species are native and appropriate for the site; and plan for post-drop monitoring. The most effective drone reforestation programs use tools like this to frame logistics, then iterate based on field results and long-term ecosystem responses.