Payload Mass Fraction Solution

STEP 0: Pre-Calculation Summary
Formula Used
Payload Mass Fraction = Payload Mass/(Propellant Mass+Structural Mass)
λ = md/(mp+ms)
This formula uses 4 Variables
Variables Used
Payload Mass Fraction - Payload Mass Fraction quantifies the portion of a rocket's total mass that is attributed to the payload.
Payload Mass - (Measured in Kilogram) - Payload Mass is the mass of the payload that the rocket carries, such as satellites, instruments, or other cargo.
Propellant Mass - (Measured in Kilogram) - Propellant Mass refers to the total mass of propellant used in a propulsion system.
Structural Mass - (Measured in Kilogram) - Structural Mass is the mass of the rocket's structure, including tanks, engines, guidance systems, and other hardware.
STEP 1: Convert Input(s) to Base Unit
Payload Mass: 34 Kilogram --> 34 Kilogram No Conversion Required
Propellant Mass: 13 Kilogram --> 13 Kilogram No Conversion Required
Structural Mass: 44 Kilogram --> 44 Kilogram No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
λ = md/(mp+ms) --> 34/(13+44)
Evaluating ... ...
λ = 0.596491228070175
STEP 3: Convert Result to Output's Unit
0.596491228070175 --> No Conversion Required
FINAL ANSWER
0.596491228070175 0.596491 <-- Payload Mass Fraction
(Calculation completed in 00.016 seconds)

Credits

Creator Image
Created by LOKESH
Sri Ramakrishna Engineering College (SREC), COIMBATORE
LOKESH has created this Calculator and 25+ more calculators!
Verifier Image
Verified by Harsh Raj
Indian Institute of Technology, Kharagpur (IIT KGP), West Bengal
Harsh Raj has verified this Calculator and 100+ more calculators!

Theory Of Rockets Calculators

Rocket Exhaust Gas Velocity
​ LaTeX ​ Go Jet Velocity = sqrt(((2*Specific Heat Ratio)/(Specific Heat Ratio-1))*[R]*Temperature at Chamber*(1-(Nozzle Exit Pressure/Pressure at Chamber)^((Specific Heat Ratio-1)/Specific Heat Ratio)))
Total Velocity Required to Place Satellite in Orbit
​ LaTeX ​ Go Total Velocity of Rocket = sqrt(([G.]*Mass Of Earth*(Radius of Earth+2*Height of Satellite))/(Radius of Earth*(Radius of Earth+Height of Satellite)))
Velocity Increment of Rocket
​ LaTeX ​ Go Velocity Increment of Rocket = Jet Velocity*ln(Initial Mass of Rocket/Final Mass of Rocket)
Structural Mass Fraction
​ LaTeX ​ Go Structural Mass Fraction = Structural Mass/(Propellant Mass+Structural Mass)

Payload Mass Fraction Formula

​LaTeX ​Go
Payload Mass Fraction = Payload Mass/(Propellant Mass+Structural Mass)
λ = md/(mp+ms)

what is Payload Mass ?

The payload mass refers to the mass of the cargo, instruments, or other useful components that a rocket carries and delivers to its intended destination. In the context of rocket engineering, the payload mass represents the primary objective of the rocket mission and is the reason for launching the rocket into space or to a specific target.

How to Calculate Payload Mass Fraction?

Payload Mass Fraction calculator uses Payload Mass Fraction = Payload Mass/(Propellant Mass+Structural Mass) to calculate the Payload Mass Fraction, Payload Mass Fraction formula is defined as the ratio of the mass of the payload to the total mass of the rocket, including the propellant and structure. It is crucial for assessing the efficiency and capability of rocket designs. Payload Mass Fraction is denoted by λ symbol.

How to calculate Payload Mass Fraction using this online calculator? To use this online calculator for Payload Mass Fraction, enter Payload Mass (md), Propellant Mass (mp) & Structural Mass (ms) and hit the calculate button. Here is how the Payload Mass Fraction calculation can be explained with given input values -> 0.596491 = 34/(13+44).

FAQ

What is Payload Mass Fraction?
Payload Mass Fraction formula is defined as the ratio of the mass of the payload to the total mass of the rocket, including the propellant and structure. It is crucial for assessing the efficiency and capability of rocket designs and is represented as λ = md/(mp+ms) or Payload Mass Fraction = Payload Mass/(Propellant Mass+Structural Mass). Payload Mass is the mass of the payload that the rocket carries, such as satellites, instruments, or other cargo, Propellant Mass refers to the total mass of propellant used in a propulsion system & Structural Mass is the mass of the rocket's structure, including tanks, engines, guidance systems, and other hardware.
How to calculate Payload Mass Fraction?
Payload Mass Fraction formula is defined as the ratio of the mass of the payload to the total mass of the rocket, including the propellant and structure. It is crucial for assessing the efficiency and capability of rocket designs is calculated using Payload Mass Fraction = Payload Mass/(Propellant Mass+Structural Mass). To calculate Payload Mass Fraction, you need Payload Mass (md), Propellant Mass (mp) & Structural Mass (ms). With our tool, you need to enter the respective value for Payload Mass, Propellant Mass & Structural Mass and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!