Research Article

Particulate Emissions Hazards Associated with Fueling Heat Engines

Table 2

NASA subsonic transport system-level metrics (From http://www.aeronautics.nasa.gov/calendar/era_preconference_synopsis.htm).

Corners of the trade space * Technology benefits relative to a single aisle reference configuration * Technology benefits relative to a large twin aisle reference configuration * Technology benefits

Noise, dB(cum. below Stage 4)−32−42−71
LTO NOx emissions, %(below CAEP 6)**−60−75Better than −75
Performance:aircraft fuel burn, %−33***−50***Better than −70
Performance:field length, %−33−50Exploit metro-plex concepts****

*Technology Readiness Level for key technologies = 4–6. N represents current aviation technology, For example, Boeing 787.
**LTO is landing-take-off cycle and CAEP is Committee on Aviation Environmental Protection.
***Recently updated. Additional gains made are possible through operational improvements.
****Concepts that enable optimal use of runways at multiple airports within the metropolitan area.