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Contents of the Rocket Propulsion PDF

List of 27 Rocket Propulsion Formulas

Acceleration of Rocket

Area Ratio of Nozzles

Characteristics Velocity

Compressible Area Ratio

Effective Exhaust Velocity of Rocket

Exit Velocity given Mach Number and Exit Temperature

Exit Velocity given Molar Mass

Exit Velocity given Molar Specific Heat Capacity

Jet Velocity

Mass Flow Rate through Engine

Mass Ratio of Rocket

Nozzle Thrust Coefficient

Payload Mass Fraction

Photon Propulsion Thrust

Power required to produce Exhaust Jet Velocity

Power required to produce Exhaust Jet Velocity given Mass of Rocket and Acceleration

Propellent Mass Fraction

Propulsion Efficiency

Rocket Exit Pressure

Rocket Exit Temperature

Structural Mass Fraction

Throat Velocity of Nozzle

Thrust given Exhaust Velocity and Mass Flow Rate

Thrust given Mass and Acceleration of Rocket

Total Impulse

Total Velocity Required to Place Satellite in Orbit

Velocity Increment of Rocket

Variables used in Rocket Propulsion PDF

a Acceleration (Meter per Square Second)
A Area (Square Meter)
A_r Area Ratio
A_t Nozzle Throat Area (Square Meter)
C_F Thrust Coefficient
C_j Exit Velocity (Meter per Second)
C_{p molar} Molar Specific Heat Capacity at Constant Pressure (Joule Per Kelvin Per Mole)
C^✸ Characteristics Velocity (Meter per Second)
DIV1 Dummy Input Variable1
DIV2 Dummy Input Variable2
DOV Dummy Output Variable
F Thrust (Newton)
F Thrust (Newton)
h Height of Satellite (Meter)
m Mass of Rocket (Kilogram)
M Mach Number
m₀ Initial Mass (Kilogram)
m_a Mass Flow Rate (Kilogram per Second)
M_e Exit Mass (Kilogram)
M_E Mass Of Earth (Kilogram)
m_f Final Mass (Kilogram)
m_f Final Mass of Rocket (Kilogram)
m_i Initial Mass of Rocket (Kilogram)
M_molar Molar Mass (Gram Per Mole)
m_p Propellant Mass (Kilogram)
MR Mass Ratio
P Power Required (Kilowatt)
P₁ Inlet Nozzle Pressure (Pascal)
P_c Chamber Pressure (Megapascal)
P_e Power in Jet (Kilowatt)
P_exit Exit Pressure (Megapascal)
P_t Total Pressure (Megapascal)
R_E Radius of Earth (Meter)
t _i Initial time (Second)
T_c Chamber Temperature (Kelvin)
T_c Chamber Temperature (Kelvin)
T_e Exit Temparature (Kelvin)
T_exit Exit Temperature (Kelvin)
t_f Final time (Second)
T_t Total Temperature (Kelvin)
T_t Total impulse (Second)
v₀ Vehicle Speed (Meter per Second)
v₉ Exhaust Speed (Meter per Second)
V_e Jet Velocity (Meter per Second)
V_e Effective Exhaust Velocity (Meter per Second)
V_j Jet Velocity of Rocket (Meter per Second)
V_T Total Velocity of Rocket (Meter per Second)
Y Specific Heat Ratio
γ Specific Heat Ratio
ΔV Velocity Increment of Rocket (Meter per Second)
ζ Propellant Mass Fraction
η_prop Propulsion Efficiency

Constants, Functions and Measurements used in Rocket Propulsion PDF

Constant: [G.], 6.67408E-11
Gravitational constant
Constant: [c], 299792458.0
Light speed in vacuum
Constant: [R], 8.31446261815324
Universal gas constant
Function: int, int(expr, arg, from, to)
The definite integral can be used to calculate net signed area, which is the area above the x -axis minus the area below the x -axis.
Function: ln, ln(Number)
The natural logarithm, also known as the logarithm to the base e, is the inverse function of the natural exponential function.
Function: sqrt, sqrt(Number)
A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number.
Measurement: Length in Meter (m)
Length Unit Conversion
Measurement: Weight in Kilogram (kg)
Weight Unit Conversion
Measurement: Time in Second (s)
Time Unit Conversion
Measurement: Temperature in Kelvin (K)
Temperature Unit Conversion
Measurement: Area in Square Meter (m²)
Area Unit Conversion
Measurement: Pressure in Megapascal (MPa), Pascal (Pa)
Pressure Unit Conversion
Measurement: Speed in Meter per Second (m/s)
Speed Unit Conversion
Measurement: Acceleration in Meter per Square Second (m/s²)
Acceleration Unit Conversion
Measurement: Power in Kilowatt (kW)
Power Unit Conversion
Measurement: Force in Newton (N)
Force Unit Conversion
Measurement: Mass Flow Rate in Kilogram per Second (kg/s)
Mass Flow Rate Unit Conversion
Measurement: Molar Mass in Gram Per Mole (g/mol)
Molar Mass Unit Conversion
Measurement: Molar Specific Heat Capacity at Constant Pressure in Joule Per Kelvin Per Mole (J/K*mol)
Molar Specific Heat Capacity at Constant Pressure Unit Conversion

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