diff --git a/core/resources/datafiles/thrustcurves/RASAero/RASAero_Motors.eng b/core/resources/datafiles/thrustcurves/RASAero/RASAero_Motors.eng
index a5d937a21..aa98b3a1a 100644
--- a/core/resources/datafiles/thrustcurves/RASAero/RASAero_Motors.eng
+++ b/core/resources/datafiles/thrustcurves/RASAero/RASAero_Motors.eng
@@ -1898,7 +1898,7 @@ G80T 29 124 4-7-10 0.0479 0.1161 AT
 G101T 29 114.3 5-8-12 0.046 0.136 AT 
 0.01 35.29
 0.02 63.97
-0.02 78.09
+0.025 78.09
 0.03 84.71
 0.04 89.96
 0.06 93.96
@@ -7314,9 +7314,9 @@ K660 54 572 7-17 1.177 1.949 CTI
 3.69 0
 ;
 ;
-K1200 54 488 7-17 0.9814 1.6319 CTI 
+K1200 54 488 7-17 0.9814 1.6319 CTI
 0.01 492.25
-0.01 1235.24
+0.015 1235.24
 0.02 1369.46
 0.05 1236.01
 0.1 1279.47
@@ -7346,7 +7346,7 @@ K1200 54 488 7-17 0.9814 1.6319 CTI
 ;
 K1440 54 572 7-17 1.1624 1.8926 CTI 
 0.01 1061.8
-0.01 2168.21
+0.015 2168.21
 0.02 2036.3
 0.07 1691.73
 0.1 1805.18
@@ -7570,7 +7570,7 @@ M1060 98 548 0 3.622 6.673 CTI
 0.2 1453
 0.24 1494
 0.38 1450
-0.38 1425
+0.43 1425
 0.5 1423
 1 1462
 1.5 1456
@@ -7704,7 +7704,7 @@ O5100 150 803 1000 13.245 23.577 CTI
 0.04 3260.42
 0.05 4001.47
 0.07 4927.78
-0.07 5483.57
+0.08 5483.57
 0.09 5817.04
 0.13 6057.88
 0.2 6206.09
@@ -8025,7 +8025,7 @@ H124_pvc 38 508 0 0.142 0.664 SRS
 0.01 198.24
 0.02 300.84
 0.03 314.34
-0.03 316
+0.035 316
 0.04 305.39
 0.08 280.35
 0.11 221.43
@@ -8055,7 +8055,7 @@ I147_pp 38 711 0 0.264 0.967 SRS
 0 194.47
 0.02 366.71
 0.03 390.09
-0.03 392.3
+0.04 392.3
 0.05 359.02
 0.07 217.4
 0.1 207.68
@@ -8078,9 +8078,9 @@ I147_pp 38 711 0 0.264 0.967 SRS
 I117_pvc 38 914 0 0.37 1.133 SRS 
 0.01 203.36
 0.02 339.95
-0.02 358.77
+0.025 358.77
 0.03 367.94
-0.03 361.47
+0.045 361.47
 0.06 277.4
 0.08 277.11
 0.15 250.99
@@ -8233,7 +8233,6 @@ J348 54 606.5 0 0.3742 1.5983 SRS
 J144_pp 38 914 0 0.37 1.133 SRS 
 0.01 301.25
 0.03 376.44
-0.03 376.86
 0.08 247.31
 0.22 273.45
 0.45 263.59
@@ -8302,7 +8301,7 @@ K347 54 911.4 0 0.7688 2.3107 SRS
 2.06 393.65
 2.13 443.69
 2.3 365.38
-2.3 292.31
+2.35 292.31
 2.4 257.92
 2.6 184.84
 2.79 124.66
@@ -10847,7 +10846,6 @@ I150 38 229 20-100 0.1718 0.3983 EM
 ;
 I160 38 280 100 0.2319 0.4867 EM 
 0.01 205.72
-0.01 192.73
 0.2 192.73
 0.4 201.39
 0.5 199.22
@@ -11301,8 +11299,8 @@ K1075RT 54 728 1000 1.314 2.541 GM
 1.8 1123.36
 2.24 0
 ;
-;
-K700RT 54 492 1000 0.90135 0.17535 GM 
+; NOTE: the total weight in RASAero is originally 0.17535, but that is smaller than the propellant weight => throws an error...
+K700RT 54 492 1000 0.90135 1.7535 GM
 0.12 534
 0.18 658.6
 0.2 725.35
@@ -12289,8 +12287,8 @@ K600F 54 403 6-10-14-100 0.68096 1.41568 KBA
 2.548 4.025
 2.653 0
 ;
-;
-L1000S 54 727.96 100 1.301 1.248 KBA 
+; NOTE: the total weight in RASAero is originally 1.248, but that is smaller than the propellant weight => throws an error...
+L1000S 54 727.96 100 1.301 2.325 KBA
 0.038 1310.24
 0.085 1090.03
 0.139 1023.97
@@ -12303,7 +12301,7 @@ L1000S 54 727.96 100 1.301 1.248 KBA
 2.179 924.878
 2.233 737.7
 2.264 847.805
-2.295 682.648
+2.285 682.648
 2.295 539.512
 2.302 649.617
 2.318 451.428
@@ -20962,8 +20960,8 @@ M1465BL 98 870 1000 4.49 9.80 GM
 4.45 334
 5.2 0
 ;
-;
-M1025WC 98 870 1000 5.33 10.1 9.80 GM
+; NOTE: original RASAero data had "M1025WC 98 870 1000 5.33 10.1 9.80 GM", but that was an entry too many => error
+M1025WC 98 870 1000 5.33 10.1 GM
 0.1 1780
 0.5 1558
 3.25 1500
@@ -21188,7 +21186,6 @@ J160 38 1219 1000 0.327926 0.544 RTW
 0.015456 262.049
 0.185471 255.442
 0.278207 240.028
-0.278207 229.017
 0.386399 251.038
 0.510046 242.23
 0.64915 213.603