Aerospace Testing Facilities in India

Aerospace Testing Facilities available in India

  Title of the Aerospace Test
Shock Tube Facility 1
  Name of the Organisation
  Name of theLab
Indian Institute of Space Science & Technology – IISST
  Place of the Lab
  Category of Aerospace Test Wind Tunnel Testing
  Sub-category of Aerospace Test Subsonic Wind Tunnel
  Year of Establisment 2015
  Test Applications
Primarily for indigenous development testing
Testing requirements of R & D organizations and other
For both aeronautics & non aeronautical applications
  Test Special Features
Driver: Cold He/H2-O2 detonation driver
Tube size : 6.4 m long driver/driven, 60mm ID
Pressure rating : 200 bar
Enthalpy range : <5.2 MJ/kg 
  Other Test Information
  Contact Person / Institution
The Director  
Indian Institute of Space Science and Technology
Valiamala P O,
Thiruvananthapuram – 695547
Phone: +91 (471) 2568452, 2568600 
Fax: +91 (471) 2568462 
Copyright 2012-16 AR&DB.
All rights reserved
Designed,Developed and Maintained by Dr.M.Madhusudhan
Principal Investigator & Associate Professor, Department of Library and Information Science
University of Delhi, Delhi-110007