
Satellite Propulsion
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Research Title
Optimization of Compressible Flow Expansion in Micro-Scale Thruster Nozzles for CubeSat Propulsion
Why Micro-Propulsion Matters for CubeSats
The rapid growth of small satellites and CubeSats has transformed space missions by enabling low-cost Earth observation, communication, and scientific exploration. However, these missions demand highly compact, lightweight, and precise propulsion systems for orbit correction, attitude control, and formation flying.
Micro-scale thrusters are essential for meeting these requirements, but their performance is often limited by complex compressible flow phenomena that arise at very small scales. Understanding and controlling these flow behaviors is critical for improving thrust efficiency and mission reliability.
Research Objective
The goal of this research is to optimize the flow expansion process in micro-scale thruster nozzles used for CubeSat propulsion.
We aim to address key questions such as:
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How does compressible flow expand within confined micro-nozzle geometries?
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What role do shocks and flow instabilities play at high expansion ratios?
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How can nozzle geometry and operating conditions be optimized for maximum efficiency?

Challenges in Micro-Scale Compressible Flow
Unlike conventional rocket nozzles, micro-thruster nozzles operate under:
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Extremely small characteristic dimensions
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High pressure and temperature gradients
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Strong compressibility effects
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Shock formation within limited expansion lengths
These factors make analytical solutions insufficient, requiring high-fidelity numerical simulations to capture real flow behavior.
Research Methodology and Simulation Approach
This study employs Computational Fluid Dynamics (CFD) using ANSYS Fluent to perform a detailed analysis of micro-thruster nozzle performance.
Key aspects of the methodology include:
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Modeling compressible, high-speed flow through converging–diverging micro-nozzles
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Simulation of both steady-state and transient flow conditions
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Investigation of varying:
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Inlet pressure and temperature
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Throat diameter and diverging angle
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Propellant properties and gas models
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This approach allows us to identify optimal operating and design conditions for micro-thruster systems.
Flow Analysis and Performance Metrics
Post-processing and analysis focus on:
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Velocity and pressure contours
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Mach number evolution along the nozzle
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Temperature distribution and thermal gradients
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Shock formation and shock–boundary layer interactions
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Expansion efficiency and thrust-related performance metrics
These insights help quantify how effectively the nozzle converts thermal energy into directed thrust.
Significance and Impact
The outcomes of this research will:
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Improve thrust efficiency and controllability of CubeSat propulsion systems
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Support the design of reliable micro-thrusters for long-duration missions
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Provide deeper understanding of high-speed compressible flow in micro-scale geometries
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Contribute to the development of scalable propulsion technologies for future small satellite platforms
This work bridges fundamental fluid dynamics with practical spacecraft propulsion design.
Opportunities for Researchers and Collaboration
We invite researchers and students interested in:
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Satellite propulsion and space systems
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Compressible flow and shock dynamics
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Micro-scale fluid mechanics
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CFD modeling and high-speed flow simulation
By joining this research effort, collaborators can contribute to next-generation space propulsion technologies that enable advanced CubeSat missions and expand access to space.
Eligibility:
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UG: B.Tech / B.E. in Energy and Power Engineering, Automobile Engineering, Environmental Engineering, Aviation/Aeronautical/Aerospace Engineering, Marine Engineering, Mechanical Engineering (pursuing/completed)
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PG: M.Tech in Energy, Automobile, Environmental, Aviation, Marine, Mechanical (pursuing/completed)
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Doctorate: Any Doctorate (pursuing/completed)
Hardware and Software Requirements:
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Operating System: Windows 10 or above
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Software: ANSYS Student Version (Mechanical / Fluent / Workbench as required)
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System Configuration: Minimum 8 GB RAM
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Storage: At least 2 GB free space for simulation files
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Internet Connection: Required for downloading resources, submitting results, and communication
Work Description:
As a CAE Engineer Intern, you will work on simulation-based engineering problems using industry-standard tools. You will be provided with:
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A structured workflow for geometry creation, meshing, and simulation
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Step-by-step setup and execution manuals
Your Responsibilities
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Create or modify geometry based on given design parameters
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Generate and refine computational mesh for accurate simulations
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Set up and run simulations using appropriate models and boundary conditions
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Analyze results such as flow behavior, pressure distribution, forces, or thermal effects
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Perform parametric studies by changing input conditions
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Document observations and compare results across different cases
Workflow and Tools
All project data and submissions will be managed through:
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ZOHO Workspace (file sharing and documentation)
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ZOHO People (attendance and progress tracking)
Support and Guidance
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Continuous technical support will be provided by our team
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Assistance available via phone or email
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Support Hours: 11:00 AM to 5:00 PM (IST)
Benefits for Intern Future:
This research provides exposure to modern computational engineering methodologies increasingly adopted across simulation, product development, and engineering consulting industries.
Traditional mechanical engineering roles have focused heavily on design, manufacturing, and conventional analysis methods. However, modern engineering industries are rapidly shifting toward:
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Simulation-Driven Product Development
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Digital Engineering and Virtual Testing
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Computational Fluid Dynamics (CFD) Analysis
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Numerical and Performance-Based Engineering Evaluation
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Design Optimization through Computational Analysis
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Simulation-Based Research and Validation
By working on practical CAE and simulation workflows, mechanical engineering students can develop hands-on understanding of modern engineering methodologies used in advanced industrial R&D and engineering consulting environments.
This experience can support future opportunities in domains such as:
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CAE and CFD Analysis
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Engineering Simulation Consulting
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Aerospace and Automotive Simulation
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Thermal and Fluid System Analysis
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Product Development and Optimization
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Computational Engineering Research
Organizations and consulting companies actively working in these areas include:
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Tata Technologies
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L&T Technology Services
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Quest Global
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Capgemini Engineering
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KPIT Technologies
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Altair Engineering
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ANSYS
As industries increasingly adopt simulation-driven engineering and digital product development methodologies, gaining early exposure to these computational workflows can help participants build stronger industry-relevant engineering and analysis-oriented profiles.