Aerospace Testing Facilities available in India
 |
||
| Title of the Aerospace Test |
Shock Tunnel Facility 2 |
|
| Name of the Organisation |
ISRO |
|
| Name of theLab |
Indian Institute of Space Science & Technology – IISST |
|
| Place of the Lab |
Thiruvananthapuram |
|
| 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 industries For both aeronautics & non aeronautical applications |
|
| Test Special Features | This is proposed as an extension to the shock tube facility. Nozzle exit dia: 250 mm Test conditions: Steady flow duration: approx4 ms (Tailored interface operation) |
|
| 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 Email: admin@iist.ac.in Website: http://www.iist.ac.in/ |
|