diff --git a/GameData/RealismOverhaul/Engine_Configs/Nike_Config.cfg b/GameData/RealismOverhaul/Engine_Configs/Nike_Config.cfg index 01a5e36069..954beb5de7 100644 --- a/GameData/RealismOverhaul/Engine_Configs/Nike_Config.cfg +++ b/GameData/RealismOverhaul/Engine_Configs/Nike_Config.cfg @@ -8,8 +8,8 @@ // Nike // // Dry Mass: 195 Kg -// Thrust (SL): 193.05 kN, calculated from total impulse / total burn time -// Thrust (Vac): 224.46 kN +// Thrust (SL): 187.37 kN, calculated from total impulse / total burn time +// Thrust (Vac): 217.96 kN // ISP: 196 SL / 228 Vac, calculated from typo'd vac thrust, and total impulse/burn time. // Burn Time: 3.4 // M5 is 3.5s, with other numbers scaled as such (42143 lbf sea level, etc) // Chamber Pressure: ??? MPa @@ -44,7 +44,6 @@ // Dry Mass: 430 lb // Thrust: 50,461.5 lb vac -- the technical data reference mentions 59klbf vac thrust for M5, which is likely a typo for 49klbf. Later it mentions 43.4klbf "vac" thrust for M5E1 but that does not jibe with other references reporting 43.4klbf takeoff thrust (technically x4, since clustered) // The NASA sources mention 42.5klbf, which again seems correct for liftoff thrust rather than vac thrust given the thing only burns 3.4-3.5s. -// So use 3.5/3.4 (which equates to 43.4/42.143) * 49,000 = 50,461.5 lbf // ================================================== @PART[*]:HAS[#engineType[Nike-M5E1]]:FOR[RealismOverhaulEngines] @@ -93,8 +92,8 @@ { name = Nike-M5E1 specLevel = operational - maxThrust = 224.46 - minThrust = 224.46 + maxThrust = 217.96 + minThrust = 217.96 heatProduction = 100 PROPELLANT { @@ -109,14 +108,14 @@ } curveResource = NGNC + //assuming two takeoff thrust references state average and peak thrust thrustCurve { key = 1.00 0.90 key = 0.99 0.95 - key = 0.96 1.0 - key = 0.92 0.999 - key = 0.89 0.998 - key = 0.63 0.960 + key = 0.96 1.005 + key = 0.89 1.03 + key = 0.63 0.995 key = 0.37 0.810 key = 0.10 0.314 key = 0.00 0.10