diff --git a/content/blog/03_quadrocopter_en.md b/content/blog/03_quadrocopter_en.md
index 10d8a88..9cba46f 100644
--- a/content/blog/03_quadrocopter_en.md
+++ b/content/blog/03_quadrocopter_en.md
@@ -37,8 +37,8 @@ would result in a higher torque at low throttle.
 Since I wanted to use motors with a actual data sheet or at least a test measurement how much thrust and
 amps would be drawn with certain types of propeller I did take a look at the [T-Motor F20II F20 II 1408 3750KV](https://www.banggood.com/T-Motor-F20II-F20-II-1406-3750KV-Brushless-Motor-2-4S-For-130-140-150-FPV-Racing-Frame-p-1154351.html)
 
-The where the ones which had a lot of thrust with XXXg when they are mounted with 3040 propeller types.
-T
+The where the ones which had a lot of thrust with 532g when they are mounted with 3040 propeller types.
+The goal of the quad would be to be below 250g so the thrust to weight ratio would be 1:8 for a quad copter.
 
 [lightgallery
     /images/quad/motor.jpg, T-Motor F20II F20 II 1408 3750KV Source: www.banggood.com;
diff --git a/pelicanconf.py b/pelicanconf.py
index e75c050..35481a8 100644
--- a/pelicanconf.py
+++ b/pelicanconf.py
@@ -42,7 +42,7 @@ EXTRA_PATH_METADATA = {
 # Base URL this page is hosted at:
 SITENAME = 'phschoen.de'
 # SITEURL = 'http://skylx125.ndsatcom.com:8000'
-SITEURL = 'http://localhost:8000'
+SITEURL = 'http://phschoen.de'
 
 # Timezone is GMT+1:
 TIMEZONE = 'Europe/Paris'