Tool · Mission profiles and weight fractions
Mission Profile Builder
Assemble a mission from segments, as sizing does: start from a typical profile or a blank one, set each segment's altitude, speed, distance or time, and see the profile drawn, its time and distance added up, and its weight fractions multiplied into the mission fuel fraction. Use it to check the examples of Lessons 5 and 6, and for your own design.
Build a mission
Start from
Segment by segment
| \(i\) | Segment | Distance (km) | Time (min) | Altitude at end (km) | \(W_i/W_{i-1}\) | \(W_i/W_0\) |
|---|
How it is calculated
| Segment | Time and distance | Weight fraction \(W_i/W_{i-1}\) |
|---|---|---|
| Warmup and takeoff | Time as entered; no distance | Historical: 0.970 |
| Climb | \(t = \Delta h/\overline{RC}\), \(d = \overline{V}t\) | Historical: 0.985 |
| Cruise | \(t = R/V\) at the current altitude | Breguet: \(\exp[-RC/(V\,L/D)]\) |
| Loiter | Time as entered; distance not counted toward the range | Endurance: \(\exp[-EC/(L/D)]\) |
| Combat | Time as entered; no distance counted | As entered; for example \(1 - C(\TW)t\) at full thrust |
| Descent | \(d = \Delta h/\tan\gamma_d\), \(t = d/\overline{V}\) | As entered (often taken as 1, counting descent fuel with the landing) |
| Landing and taxi | Time as entered; no distance | Historical: 0.995 |
The mission fraction is the product \(W_x/W_0 = \prod W_i/W_{i-1}\), and the fuel fraction with the 6% allowance for reserve and trapped fuel is \(\Wf/\Wo = 1.06(1 - W_x/W_0)\). If the profile already contains explicit reserve segments (a diversion, a hold), the allowance double-counts part of the reserve: switch it off to see the difference. The tool does not model weight dropped in flight (weapons released, cargo air-dropped); Module 3 shows how. Your mission is saved in this browser, so it is still here when you come back.
See Lesson 5 for the profiles and the timeline, and Lesson 6 for reserves and the endurance equation.