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Hall Effect Thruster (HET) Electric Propulsion Thrust & Efficiency Calculator

Easily calculate and compute hall effect thruster (het) electric propulsion thrust & efficiency calculator with accurate equations, live formulas, and expert guidance.

Calculated Result
96.09 mN

Electric Thrust Output (T_thrust)

Electric Thrust Output (T_thrust)

96.09 mN

Thrust Milli Newtons

96.08852168842182

Specific Impulse Sec

1884.288912437789

Thrust To Power Ratio M N Per Kw

71.17668273216431

Total Thrust Efficiency Percent

65.76213675403353

96.09 — mN

Calculation Breakdown

  1. Applied FormulaModels plasma acceleration in Hall Effect Thrusters (SPT / TAL), calculating electromagnetic thrust (mN), specific impulse (Isp > 1500 s), and total electrical-to-kinetic thrust efficiency (eta_T %).T = \sqrt{2 \dot{m}_i \frac{e}{M} V_d} \approx \sqrt{2 \dot{m} P_{\text{thrust}}}, \quad \eta_T = \frac{T^2}{2 \dot{m} P_{\text{elec}}} = \frac{1}{2} \frac{T \cdot I_{\text{sp}} g_0}{P_{\text{elec}}}

Hall Thruster Thrust & Efficiency Metric Output

Interactive visualization based on your current inputs

Calculated Value
0.024487296Electric Thrust Output (T_thrust)

What Is the Hall Effect Thruster (HET) Electric Propulsion Thrust & Efficiency Calculator?

The Hall Effect Thruster (HET) Electric Propulsion Thrust & Efficiency Calculator computes results using established domain formulas, verified conversion factors, and user-entered parameters.

How Does the Hall Effect Thruster (HET) Electric Propulsion Thrust & Efficiency Calculator Work?

Models plasma acceleration in Hall Effect Thrusters (SPT / TAL), calculating electromagnetic thrust (mN), specific impulse (Isp > 1500 s), and total electrical-to-kinetic thrust efficiency (eta_T %).

Hall Effect Thruster (HET) Electric Propulsion Thrust & Efficiency Calculator Formula & Variables

The core mathematical equation utilized by this calculator is expressed as:

T=2m˙ieMVd≈2m˙Pthrust,ηT=T22m˙Pelec=12T⋅Ispg0PelecT = \sqrt{2 \dot{m}_i \frac{e}{M} V_d} \approx \sqrt{2 \dot{m} P_{\text{thrust}}}, \quad \eta_T = \frac{T^2}{2 \dot{m} P_{\text{elec}}} = \frac{1}{2} \frac{T \cdot I_{\text{sp}} g_0}{P_{\text{elec}}}

Models plasma acceleration in Hall Effect Thrusters (SPT / TAL), calculating electromagnetic thrust (mN), specific impulse (Isp > 1500 s), and total electrical-to-kinetic thrust efficiency (eta_T %).

How to Use the Hall Effect Thruster (HET) Electric Propulsion Thrust & Efficiency Calculator

  1. Enter your parameters into the designated input fields to calculate the result immediately.

Step-by-Step Example Calculation

Hall Effect Thruster (HET) Electric Propulsion Thrust & Efficiency Calculator Example

Input Values:

dischargeVoltageVolts:300
dischargeCurrentAmps:4.5
xenonMassFlowRateMgS:5.2
massUtilizationEfficiencyPct:88
Worked Steps: Sample evaluation based on standard reference conditions.

Understanding Your Result

The calculated primary figure indicates the optimal or required mN.

Factors That Affect the Result

  • Measurement tolerances, operational variance, and real-world conditions.

When Should You Use This Calculator?

  • Everyday budgeting, technical homework, professional estimation, and household projects.

Assumptions & Limitations

  • Assumes standard atmospheric or environmental parameters unless specified.

Frequently Asked Questions

Calculation Accuracy & Reference Note

Double-precision IEEE 754 arithmetic with validated empirical constants.

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