<commit_before># -*- coding: utf-8 -*-
"""
Python Flight Mechanics Engine (PyFME).
Copyright (c) AeroPython Development Team.
Distributed under the terms of the MIT License.

Constant variables
------------------

"""

# AIR CONSTANTS

GAMMA_AIR = 1.4   								# Adiabatic index or ratio of specific heats (dry air at 20º C)
R_AIR = 287.05287  								# Specific gas constant for dry air - J/(Kg·K)

# Air at sea level conditions h=0 (m)

RHO_0 = 1.225 					 				# Density at sea level (kg/m3)
P_0 = 101325  							       	# Pressure at sea level (Pa)
SOUND_VEL_0 = 340.293990543  					# Sound speed at sea level (m/s)


# EARTH CONSTANTS

GRAVITY = 9.80665  								# Gravity of Ethe Earth - m/s^2
STD_GRAVITATIONAL_PARAMETER = 3.986004418e14    # Standard Gravitational Parameter is the product of the gravitational
												# constant G and the mass M of the body - m³/s²
EARTH_MASS = 5.9722e24  						# Mass of the Earth - kg
GRAVITATIONAL_CONSTANT = 6.67384e11 			# Gravitational constant - N·m²/kg²
EARTH_MEAN_RADIUS = 6371000 					# Mean radius of the Earth - m


# CONVERSIONS

lbs2kg = 0.453592								# Pounds (lb) to kilograms (kg)
ft2m = 0.3048									# Feet (ft) to meters (m)
slug2kg = 14.5939								# Slug to kilograms (kg)
slugft2_2_kgm2 = 1.35581795						# Slug*feet^2 to kilograms*meters^2 (kg*m^2)<commit_msg>Fixed issue with tabs and spaces in constants file<commit_after># -*- coding: utf-8 -*-
"""
Python Flight Mechanics Engine (PyFME).
Copyright (c) AeroPython Development Team.
Distributed under the terms of the MIT License.

Constant variables
------------------

"""

# AIR CONSTANTS

GAMMA_AIR = 1.4  # Adiabatic index or ratio of specific heats (dry air at 20º C)
R_AIR = 287.05287  # Specific gas constant for dry air - J/(Kg·K)

# Air at sea level conditions h=0 (m)

RHO_0 = 1.225  # Density at sea level (kg/m3)
P_0 = 101325  # Pressure at sea level (Pa)
SOUND_VEL_0 = 340.293990543  # Sound speed at sea level (m/s)


# EARTH CONSTANTS

GRAVITY = 9.80665  # Gravity of Ethe Earth - m/s^2
STD_GRAVITATIONAL_PARAMETER = 3.986004418e14  # Standard Gravitational Parameter is the product of the gravitational
# constant G and the mass M of the body - m³/s²
EARTH_MASS = 5.9722e24  # Mass of the Earth - kg
GRAVITATIONAL_CONSTANT = 6.67384e11  # Gravitational constant - N·m²/kg²
EARTH_MEAN_RADIUS = 6371000  # Mean radius of the Earth - m


# CONVERSIONS

lbs2kg = 0.453592  # Pounds (lb) to kilograms (kg)
ft2m = 0.3048  # Feet (ft) to meters (m)
slug2kg = 14.5939  # Slug to kilograms (kg)
slugft2_2_kgm2 = 1.35581795  # Slug*feet^2 to kilograms*meters^2 (kg*m^2)
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