jsbsim.js
Version:
JSBSim flight dynamics model ported to JavaScript
18 lines (16 loc) • 448 B
text/xml
<FG_ROCKET NAME="LM_Descent">
<!--
SHR = Specific Heat Ratio, for LOX/Ammonia this is 1.23
MAX_PC = Maximum chamber pressure in psf
PROP_EFF = propulsive efficiency. This is largely a fudge factor.
-->
SHR 1.24
MAX_PC 15840.0
VARIANCE 0.10
PROP_EFF 0.67
MAXTHROTTLE 1.0
MINTHROTTLE 0.1
SLFUELFLOWMAX 34.0
SLOXIFLOWMAX 34.0
</FG_ROCKET>