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Download the Plane Maker Manual - X-Plane

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60 4. WORKING WITH THE AIRCRAFT’S SYSTEMS<br />

efficient inlet speed.<br />

At <strong>the</strong> top of <strong>the</strong> middle column in <strong>the</strong> Jet Engine Specs box is <strong>the</strong> compressor area, given<br />

in square feet. Specifically, this is <strong>the</strong> frontal area of <strong>the</strong> engine compressor, calculated as π times<br />

<strong>the</strong> radius of <strong>the</strong> compressor for engines with <strong>the</strong> whole of <strong>the</strong>ir (round) compressors open to drag<br />

effects. The compressor’s frontal area only has a significant effect on drag at low throttle settings.<br />

Beneath <strong>the</strong> compressor area is <strong>the</strong> minimum N1 for fuel introduction, set as a percentage of<br />

N1’s maximum speed. If fuel is introduced into <strong>the</strong> engine prior to this speed, a hot start (a start<br />

that exceeds <strong>the</strong> maximum temperature <strong>the</strong> engine is designed to handle) may ensue. Beneath <strong>the</strong><br />

minimum N1 is <strong>the</strong> fan RPM at 100% N1, measured in rotations per minute.<br />

At <strong>the</strong> top of <strong>the</strong> far right column in <strong>the</strong> Jet Engine Specs box is <strong>the</strong> “engine-start fuel intro<br />

time”-<strong>the</strong> time, in seconds, that it takes to go from no fuel to idle fuel flow during <strong>the</strong> engine’s<br />

starting process.<br />

Beneath <strong>the</strong> fuel intro time is <strong>the</strong> “throttle advance time from idle to maximum.” This sets <strong>the</strong><br />

time in seconds that it takes <strong>the</strong> engine to go from idle to full torque if <strong>the</strong> throttle is commanded<br />

instantly from idle to full. It is, more accurately, <strong>the</strong> time it takes N1 to bring in torque when <strong>the</strong><br />

throttle is moved to full.<br />

The final parameter in <strong>the</strong> Jet Engine Specs box is <strong>the</strong> thrust-reverser deployment time, <strong>the</strong><br />

time in seconds that it takes <strong>the</strong> thrust reverser to deploy and retract.<br />

Working with Rocket Engines<br />

Rocket engines, like jets, are quite simple to set up in <strong>Plane</strong> <strong>Maker</strong>. Use <strong>the</strong> Location tab of <strong>the</strong><br />

Engine Specs dialog box to set <strong>the</strong> position of <strong>the</strong> center of <strong>the</strong> engine’s thrust (as described in<br />

<strong>the</strong> section “Features Shared by All Engine Types” above). For a jet engine, this center of thrust<br />

is usually <strong>the</strong> center of <strong>the</strong> exhaust nozzle. Check <strong>the</strong> “vectors” box in that tab if <strong>the</strong> engine will<br />

vector.<br />

After setting <strong>the</strong> rocket engine’s location, you can set its o<strong>the</strong>r characteristics using <strong>the</strong> “Rocket<br />

Engine Specs” box (seen in Figure 4.15), located in <strong>the</strong> Description tab of <strong>the</strong> Engine Specs dialog<br />

box.<br />

Figure 4.15: The Rocket Engine Specs portion of <strong>the</strong> Description tab<br />

Here, <strong>the</strong>re are three parameter boxes for thrust. From left to right, <strong>the</strong>se set <strong>the</strong> maximum<br />

thrust of <strong>the</strong> rocket engine, in pounds,<br />

• at sea level,<br />

• at <strong>the</strong> engine’s design altitude, and<br />

• in a vacuum.<br />

In X-<strong>Plane</strong>, <strong>the</strong> engine can put out full thrust in all three conditions, though real rockets are<br />

not always able to do so.

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