diff --git a/Model/Propulsion/__pycache__/power_comp.cpython-36.pyc b/Model/Propulsion/__pycache__/power_comp.cpython-36.pyc
index 98ccae6..663225d 100644
Binary files a/Model/Propulsion/__pycache__/power_comp.cpython-36.pyc and b/Model/Propulsion/__pycache__/power_comp.cpython-36.pyc differ
diff --git a/Model/Propulsion/power_comp.py b/Model/Propulsion/power_comp.py
index 4b96418..0d83a25 100644
--- a/Model/Propulsion/power_comp.py
+++ b/Model/Propulsion/power_comp.py
@@ -1,9 +1,9 @@
 from openmdao.api import ExplicitComponent
 
+n = 1 # variable accounting for failed motor and e extra power
 
 class PowerComp(ExplicitComponent):
-
-
+    
  
 
     def setup(self):
@@ -30,7 +30,7 @@ def compute(self, inputs, outputs):
 
 
         S = 3.14*(r**2)
-        T = W/8 # thrust required per motor
+        T = n*W/8 # thrust required per motor
         ct = T/( rho *S* (tip_speed**2) )
         cp = ( 1.15*( (ct**(3/2)) /(2**.5) ) + (1/8)*0.1*cd0 )
         PI = T * ((T/(2*S*rho))**.5)
diff --git a/solver.py b/solver.py
index 7d764ff..b9c98f7 100644
--- a/solver.py
+++ b/solver.py
@@ -42,8 +42,8 @@
 prob.driver.options['disp'] = True
 
 model.add_design_var('r',lower=0.5,upper=1.5)
-model.add_design_var('We/W0',lower=0.50,upper=0.80)
-model.add_constraint('weight.W0',lower = 2000,upper=2500)
+model.add_design_var('We/W0',lower=0.30,upper=0.70) # 30% - 70%, from lecture
+model.add_constraint('weight.W0',lower = 1500,upper=2500)
 model.add_constraint('FOM.FM',equals=0.80)
 model.add_objective('FOM.PH')