681
edits
Legoboyvdlp (talk | contribs) (→Notes) |
m (→Notes: add dead link notice) |
||
Line 309: | Line 309: | ||
*This model can only be used with the "direct" thruster. See the file: /engine/direct.xml | *This model can only be used with the "direct" thruster. See the file: /engine/direct.xml | ||
*TSFC=fuel consumption per hour/thrust | *TSFC=fuel consumption per hour/thrust | ||
*There is a Java program here to calculate thrust vs airspeed and altitude. http://adg.stanford.edu/aa241/propulsion/engmodel.html | *There is a Java program here to calculate thrust vs airspeed and altitude. http://adg.stanford.edu/aa241/propulsion/engmodel.html<nowiki/>{{Dead link}} | ||
* n1spinup and n2spinup are the rate (in %/sec) of increase below 25.8% N2, or until 15% if cutoff is false. These N% values can be manipulated by ignitionn1 and ignitionn2. | * n1spinup and n2spinup are the rate (in %/sec) of increase below 25.8% N2, or until 15% if cutoff is false. These N% values can be manipulated by ignitionn1 and ignitionn2. | ||
* acceleration between 25.8% N2 and Idle is at a preset rate of 2.0/%sec for M2, 1.4%/sec for N1. Can now be manipulated by n1startrate / n2startrate | * acceleration between 25.8% N2 and Idle is at a preset rate of 2.0/%sec for M2, 1.4%/sec for N1. Can now be manipulated by n1startrate / n2startrate |
edits