diff --git a/ThrustCurve.png b/ThrustCurve.png
index ac42fec..f004877 100644
Binary files a/ThrustCurve.png and b/ThrustCurve.png differ
diff --git a/readme.md b/readme.md
index 9531269..6ae3d7c 100644
--- a/readme.md
+++ b/readme.md
@@ -1,8 +1,13 @@
 # Air Prop Thrust 
-Total Impulse: 405.0 ± 39.0 N s
+
+Total Impulse: 405.0 ± 40.0 N s
+
+Burn TIme: 16.041999999996623 s
 
 ![Thrust Over Time](ThrustCurve.png)
 
 More Data:
 
-<table class="data-frame"><thead><tr><th></th><th>variable</th><th>mean</th><th>min</th><th>median</th><th>max</th><th>nmissing</th><th>eltype</th></tr><tr><th></th><th>Symbol</th><th>Quantity</th><th>Quantity</th><th>Quantity</th><th>Quantity</th><th>Int64</th><th>DataType</th></tr></thead><tbody><p>4 rows × 7 columns</p><tr><th>1</th><td>Thrust</td><td>69.0±6.7 N</td><td>0.0±0.0 N</td><td>86.7±9.2 N</td><td>86.7±9.2 N</td><td>0</td><td>Quantity{Measurement{Float64}, 𝐋 𝐌 𝐓^-2, FreeUnits{(N,), 𝐋 𝐌 𝐓^-2, nothing}}</td></tr><tr><th>2</th><td>Pressure</td><td>1.21e7±2.0e6 Pa</td><td>620000.0±440000.0 Pa</td><td>1.12e7±2.8e6 Pa</td><td>2.9e7±2.1e6 Pa</td><td>0</td><td>Quantity{Measurement{Float64}, 𝐌 𝐋^-1 𝐓^-2, FreeUnits{(Pa,), 𝐌 𝐋^-1 𝐓^-2, nothing}}</td></tr><tr><th>3</th><td>Time</td><td>2.9325 s</td><td>0.0 s</td><td>2.9325 s</td><td>5.865 s</td><td>0</td><td>Quantity{Float64, 𝐓, FreeUnits{(s,), 𝐓, nothing}}</td></tr><tr><th>4</th><td>Mass</td><td>0.196±0.043 kg</td><td>0.01±0.0077 kg</td><td>0.181±0.054 kg</td><td>0.468±0.053 kg</td><td>0</td><td>Quantity{Measurement{Float64}, 𝐌, FreeUnits{(kg,), 𝐌, nothing}}</td></tr></tbody></table>
+<table class="data-frame"><thead><tr><th></th><th>variable</th><th>mean</th><th>min</th><th>median</th><th>max</th><th>nmissing</th><th>eltype</th></tr><tr><th></th><th>Symbol</th><th>Quantity</th><th>Quantity</th><th>Quantity</th><th>Quantity</th><th>Int64</th><th>DataType</th></tr></thead><tbody><p>4 rows × 7 columns</p><tr><th>1</th><td>Thrust</td><td>25.3±2.5 N</td><td>0.0±0.0 N</td><td>26.7±5.9 N</td><td>26.7±5.9 N</td><td>0</td><td>Quantity{Measurement{Float64}, 𝐋 𝐌 𝐓^-2, FreeUnits{(N,), 𝐋 𝐌 𝐓^-2, nothing}}</td></tr><tr><th>2</th><td>Pressure</td><td>1.39e7±3.6e6 Pa</td><td>300000.0±1.1e6 Pa</td><td>1.38e7±3.9e6 Pa</td><td>2.9e7±2.1e6 Pa</td><td>0</td><td>Quantity{Measurement{Float64}, 𝐌 𝐋^-1 𝐓^-2, FreeUnits{(Pa,), 𝐌 𝐋^-1 𝐓^-2, nothing}}</td></tr><tr><th>3</th><td>Time</td><td>8.021 s</td><td>0.0 s</td><td>8.021 s</td><td>16.042 s</td><td>0</td><td>Quantity{Float64, 𝐓, FreeUnits{(s,), 𝐓, nothing}}</td></tr><tr><th>4</th><td>Mass</td><td>0.225±0.065 kg</td><td>0.005±0.018 kg</td><td>0.224±0.071 kg</td><td>0.468±0.053 kg</td><td>0</td><td>Quantity{Measurement{Float64}, 𝐌, FreeUnits{(kg,), 𝐌, nothing}}</td></tr></tbody></table>
+
+`readme auto generated`
diff --git a/thrust.jl b/thrust.jl
index 6e5e423..7668d59 100644
--- a/thrust.jl
+++ b/thrust.jl
@@ -2,7 +2,6 @@ using Unitful
 using DataFrames
 using Plots
 using UnitfulRecipes
-using Roots
 using CSV
 using Measurements
 using Printf
@@ -12,14 +11,13 @@ using Printf
 V = (85 ± 5)u"inch^3"
 P0 = (4200.0 ± 300)u"psi"
 Wtank = (2.3 ± 0.2)u"lb"
-Pmax = (800 ± 50)u"psi"
+Pmax = (250 ± 50)u"psi" # Max Pressure that can come out the nozzle
 
 Wsolenoid = 1.5u"kg"
 
 # Params
 d_nozzle = ((1 // 16) ± 0.001)u"inch"
 a_nozzle = (pi / 4) * d_nozzle^2
-Poutmax = (800 ± 50)u"psi"
 
 # Universal Stuff
 P_amb = (1 ± 0.2)u"atm"
@@ -34,7 +32,7 @@ M = V * (P / (R * T)) |> u"kg"
 ts = 1u"ms"
 df = DataFrame(Thrust = (0 ± 0)u"N", Pressure = P, Time = t, Mass = M)
 
-while M > 0.01u"kg"
+while M > 0.005u"kg"
     # while t < 30u"s"
     # Calculate what is leaving tank
     P = minimum([P, Pmax])
@@ -52,7 +50,7 @@ while M > 0.01u"kg"
     df_step = DataFrame(Thrust = Thrust, Pressure = P, Time = t, Mass = M)
     append!(df, df_step)
 end
-
+final_time = t |> u"s"
 impulse = sum(df.Thrust) * ts |> u"N*s"
 println("---------------------------\n\n\n\n")
 println("Total Impulse: ", impulse)
@@ -63,7 +61,7 @@ println("Mass Total: ", Wtank + Wsolenoid + maximum(df.Mass))
 
 print(describe(df))
 
-plot(df.Time[1:150:end], df.Thrust[1:150:end], title = "Thrust Over Time")
+plot(df.Time[1:350:end], df.Thrust[1:350:end], title = "Thrust Over Time")
 
 ### Save data to readme.md
 
@@ -77,13 +75,20 @@ table = String(take!(b)); # https://stackoverflow.com/a/60443621/8774114
 
 readme = Printf.@sprintf """
 # Air Prop Thrust 
+
 Total Impulse: %s
 
+Burn TIme: %s
+
 ![Thrust Over Time](ThrustCurve.png)
 
 More Data:
 
 %s
-""" impulse table
+
+`readme auto generated`
+""" impulse final_time table
+
+println(readme)
 
 write("readme.md", readme)
\ No newline at end of file