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Project MSSA-80: Mid-Size Supersonic Commercial Airliner

Python: 3.8+ DOI Status Type


Project MSSA-80 is an open-source analytical conceptual design framework for an 80-seat commercial supersonic transport jet optimized for trans-Atlantic ranges (4,200 nm) cruising at Mach 1.7.

By leveraging Advanced Composite Materials (ACMs), aeroelastic tailoring, and modern non-afterburning Variable-Cycle Engine architecture, this model demonstrates physical and financial feasibility capable of breaking even at 1.2x current international Business Class ticket pricing.


🚀 Core Architectural Parameters

  • Capacity: 80 Seats (1-1 Single-Aisle layout using deep-cradle premium ergonomic recliners).
  • Speed/Range: Mach 1.7 Cruise Velocity at 55,000–60,000 ft / 4,200 Nautical Miles.
  • Structural Composites: Carbon Fiber Reinforced Polymers (CFRP) bound with high-temperature Bismaleimide (BMI) matrix resins.
  • Propulsion: Twin Non-Afterburning Variable-Cycle Engines (Dual high-bypass subsonic / low-bypass turbojet cruise cycles).
  • Mishap-Resilient Fuel System: Polymer-blended anti-misting Sustainable Aviation Fuel (SAF) paired with inline high-shear mechanical degraders.

📊 Analytical Simulation Core

The repository contains an analytical simulation script (mssa_80_simulation.py) mapping out compressible wave drag, thermal stagnation boundary layer heating, and pressure vessel skin stress cycles across a multi-regime velocity index.

Running the Verification Model

To set up dependencies and run the core calculation simulation, deploy the following local execution context:

# Clone the Core Architecture Repository
git clone [https://github.com/Abhishek1033ubuntu/project-mssa-80.git](https://github.com/Abhishek1033ubuntu/project-mssa-80.git)
cd project-mssa-80

# Install Open-Source Computation Stack
pip install -r requirements.txt

# Run Analytical Aero-Thermal Validation Engine
python mssa_80_simulation.py

---
# Important Notice

This repository contains code published for demonstration and testing purposes only. 
The underlying intellectual property (IP) — including inventions, processes, methods, 
algorithms, and research results — is proprietary and protected under Indian law and 
international treaties (Berne Convention, Paris Convention, TRIPS Agreement).

By accessing this repository, you agree:
- The code may be viewed and studied for non-commercial, educational, or research use only.
- Any reproduction, modification, distribution, or commercialization of the IP is strictly prohibited.
- Enforcement of rights will be pursued under Indian jurisdiction and applicable international treaties.

For licensing inquiries or commercial permissions, please contact:
Abhishek Singh  | UIDAI: 9414 9122 9013
Email: abhishek1033@gmail.com | abhishek.s@live.in
Location: Madhya Pradesh, India

Note on References & IP: Detailed citations and literature references are restricted to protect Intellectual Property. See References.md for details or to request access.

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Conceptual Technical Feasibility and Economic Viability Analysis of a Next-Generation Mid-Size Supersonic Commercial Airliner Utilizing Advanced Composite Structural Architectures

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