FIELD OF THE INVENTION: The present invention relates to the field of low pressure module of a steam turbine. Particularly, the present invention relates to low pressure module capable of being used along with water cooled condenser and air cooled condenser. TERMINOLOGY & FORMULAS USED: U-Peripheral velocity of rotor; C-Steam velocity; Ct-Tangential steam velocity; Ca-Axial Steam velocity; and Delta h- Enthalpy change. The formulas employed in doing mean line calculations are as follows: 1) Loading coefficient-Delta h/U2 2) Peripheral velocity of rotor (U) = 3.147*D*N/60000 m/s Where D=Rotor Hub Dia; N=speed of rotor in rpm. 3) Steam velocity C- 44.7 *(Delta h)° 5 4) Height of the blades in a stage (H) = 2 Q/3.147*D*sina*e*C Where Q=Volumetric flow rate in each stage (m3 /sec); D= Rotor Hub Dia; a= Blade or Nozzle Inlet angle; e=Degree of admission(Projected Area of nozzles/Total area of moving blades); C=Steam velocity (Ca-Axial velocity, Ct-Tangential velocity). 5) Flow coefficient- Ca/U. DEFINITIONS OF TERMS USED: Meridional Plane: A plane cutting the turbo machine through diametric line and longitudinal axis. Pitch: Circumference of the blade (2*Pi*r)/No.of blades in a row. Circumference of the blade depends on blade height (i.e., at hub, mean or tip). Stage: Stage herein refers to a combination of blades and nozzles. Reaction: Enthalpy drop across the rows of blades/ Enthalpy drop across the stage. Lean: The angle at which the nozzles are placed with respect to vertical in nozzle diaphragm. Spanwise Reaction: Reaction across different cross-section of blade length. BACKGROUND OF THE INVENTION: Figure 1 illustrates a sectional view of two adjacent moving blades depicting typical blade features. The airfoil sections of two adjacent moving blades (10 and 12) is disclosed wherein the blades include a convex suction side (14 and 16), a concave pressure side (18 and 20), a leading edge (22 and 24) and a trailing edge (26 and 28). The parameters which define the geometry and configuration of the moving blades in a row are as follows: The distance between trailing edges (26 and 28) of two adjacent blades (10 and 12) typically referred to as pitch is indicated by a letter 'PI'. The axial length of the blade typically referred to as width is indicated by a letter 'Wl'. The inlet and exit blade angles are indicated by letters