```html
<table>
  <thead>
    <tr>
      <th>Speed (mph)</th>
      <th>Estimated thrust (N)</th>
      <th>Estimated power draw (kW)</th>
    </tr>
  </thead>
  <tbody>
    <tr>
      <td>0.0</td>
      <td>3200</td>
      <td>3.20</td>
    </tr>
    <tr>
      <td>0.5</td>
      <td>2580</td>
      <td>2.88</td>
    </tr>
    <tr>
      <td>1.0</td>
      <td>1750</td>
      <td>2.16</td>
    </tr>
    <tr>
      <td>1.5</td>
      <td>700</td>
      <td>0.94</td>
    </tr>
  </tbody>
</table>

<!--
Model/assumptions used for these estimates (very approximate):
- Actuator-disk (momentum) model, seawater density ρ = 1025 kg/m³
- Prop diameter D = 2.5 m (disk area A ≈ 4.91 m²)
- Static point used to calibrate: T0 = 3200 N at P0 = 3.2 kW
- Implied static induced velocity vi0 ≈ 0.564 m/s and overall efficiency η ≈ 0.564
- To represent thrust drop with speed for a fixed-RPM, low-pitch “mixer” style prop,
  induced velocity is forced to decrease linearly with advance speed and reaches ~0 at ~1.8 mph:
  vi(V) = vi0 * (1 - V/0.8 m/s), clipped at vi ≥ 0
- Then: T = 2 ρ A vi (V + vi) and Pshaft ≈ [T (V + vi)] / η
-->
```