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== FGTurboprop == | == FGTurboprop == | ||
The turboprop engine | The turboprop engine | ||
<h3>Configuration parameters:</h3> | |||
<pre> | |||
milthrust [LBS] | |||
idlen1 [%] | |||
maxn1 [%] | |||
betarangeend[%] | |||
if ThrottleCmd < betarangeend/100.0 then engine power=idle, propeller pitch | |||
is controled by ThrottleCmd (between MINPITCH and REVERSEPITCH). | |||
if ThrottleCmd > betarangeend/100.0 then engine power increases up to max | |||
reverse power reversemaxpower [%] max engine power in reverse mode | |||
maxpower [HP] | |||
psfc power specific fuel consumption [pph/HP] for N1=100% | |||
n1idle_max_delay [-] time constant for N1 change | |||
maxstartenginetime [sec] | |||
after this time the automatic starting cycle is interrupted when the engine | |||
doesn't start (0=automatic starting not present) | |||
startern1 [%] | |||
when starting starter spin up engine to this spin | |||
ielumaxtorque [lb.ft] | |||
if torque>ielumaxtorque limiters decrease the throttle | |||
(ielu = Integrated Electronic Limiter Unit) | |||
itt_delay [-] time constant for ITT change | |||
(ITT = Inter Turbine Temperature) | |||
</pre> | |||
== FGRocket == | == FGRocket == | ||
The rocket engine | The rocket engine |
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