Industrial Consultancy & Sponsored Research (IC&SR) , IIT Madras

Two-stage Design Based High Speed Gas Gun

Categories for this Invention

Category – Ballistic Testing Equipment

Applications – Aerospace, Military and Defense, Automotive

Industry – Aerospace Engineering, Automotive Manufacturing

Market – The global Test and Measurement Equipment market size was valued at USD 31922.18 Million in 2022 and will reach USD 63925.62 Million in 2028, with a CAGR of 12.27% during 2022-2028.

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Problem Statement

  • Existing high-speed gas guns lack efficiency and precision in achieving desired pressure and velocity profiles.
  • A two-stage design gas gun is sought to optimize pressure and velocity control for enhanced experimental accuracy and efficiency.

Technology

Two-stage design:

  • Utilizes a two-stage gas gun mechanism for firing projectiles at high velocities, enhancing efficiency and control.

Pneumatic reservoir:

  • Charges with high-pressure air to propel projectiles, providing a safer alternative to explosives.

Diaphragm rupture:

  • Controlled diaphragm rupture at predetermined pressure levels enables precise propulsion of projectiles.

Pneumatic actuator:

  • Regulates airflow between primary and secondary chambers, ensuring controlled acceleration of projectiles.

Use of light gases:

  • Utilizes light gases like hydrogen, helium, or atmospheric air as working fluids, optimizing efficiency and safety in ballistic testing.

Key Features / Value Proposition

User perspective:

  • It provides a safer and more cost-effective solution for researchers and engineers involved in ballistic resistance characterization, reducing risks associated with explosives and complexity.

Technical perspective:

  • Implements a novel two-stage gas gun design coupled with predictive capabilities, enhancing accuracy and efficiency in characterizing materials’ ballistic limits and dynamic behavior.

Questions about this Technology?

Contact For Licensing

sm-marketing@imail.iitm.ac.in
ipoffice2@iitm.ac.in

Research Lab

Prof. Velmurugan R

Department of Aerospace Engineering

Prof. Jayaganthan

Department of Engineering Design

Intellectual Property

  • IITM IDF Ref. 1900
  • IN 479752 (Patent Granted)

Technology Readiness Level

TRL- 4 Technology validated in lab scale.

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