Case I:
Thrust = Force = 100 N
Area, A = 25 cm^2
=0.0025 m^2
Pressure = Force / Area
= 100 / 0.0025
=40000 Pa
Case II:
Thrust = Force = 25 N
Area, A = 25 cm^2
=0.0025 m^2
Pressure = Force / Area
= 25 / 0.0025
=10000 Pa
Change in pressure = 40000 - 10000 = 30000 Pa