Adil Khan 11 months ago
AdiKhanOfficial #FYP Ideas

DESIGN AND DEVELOPMENT OF GIMBALLING SYSTEM USING REACTION CONTROL SYSTEM

A Vernier thruster is a rocket engine used on a spacecraft for fine adjustments to the attitude or velocity of a spacecraft. The aim of this project is to demonstrate thrust vectoring on a spacecraft using Vernier engines and maneuver the spacecraft to a certain de

Project Title

DESIGN AND DEVELOPMENT OF GIMBALLING SYSTEM USING REACTION CONTROL SYSTEM

Project Area of Specialization

Mechanical Engineering

Project Summary

A Vernier thruster is a rocket engine used on a spacecraft for fine adjustments to the attitude or velocity of a spacecraft. The aim of this project is to demonstrate thrust vectoring on a spacecraft using Vernier engines and maneuver the spacecraft to a certain degree for yaw, pitch and roll. The spacecraft chosen is Pakistan’s Ghauri missile. The fins in the original model are removed and Vernier engines will be used for thrust vectoring mechanism. Four Vernier engines will be attached at the aft end of the missile.

Project Objectives

  • Conceptual design of Vernier engine
  • 3-D Model
  • Controller Design
  • Simulation
  • Prototype
  • Testing

Project Implementation Method

The following steps are to be followed for the design and development of vernier engines:

  1. Literature review for use for vernier engines in previous spacecrafts.
  2. Ghauri missile calculations
  3. Each component’s weight calculation
  4. Calculation of center of gravity
  5. Conceptual Design of Vernier engine
  6. Configuration of engines
  7. Number of engines to be used
  8. Maneuver Selection
  9. Thrust calculation
  10. Combustion chamber and nozzle design
  11. CATIA Model
  12. Controller Design
  13. Stability Derivatives Calculation
  14. Mathematical Model
  15. Autopilot Design
  16. Simulation
  17. Prototype
  18. Mechanical Drawings
  19. Fabrication
  20. Testing

Benefits of the Project

Thrust vectoring of Ghauri missile using vernier engines.

Technical Details of Final Deliverable

Prototype of vernier engine( combustion chamber+ nozzle).

Testing for pitch, yaw movement,

Final Deliverable of the Project

HW/SW integrated system

Core Industry

Manufacturing

Other Industries

Core Technology

Others

Other Technologies

Sustainable Development Goals

Industry, Innovation and Infrastructure

Required Resources

Item Name Type No. of Units Per Unit Cost (in Rs) Total (in Rs)
Actuator Equipment4600024000
EDF Thruster Equipment4600024000
Motor Equipment410004000
Total in (Rs) 52000
If you need this project, please contact me on contact@adikhanofficial.com
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