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Departments  >>  Space Engineering and Rocketry  >  Laboratory Facilities

Aerodynamics Laboratory

Sl. No.

Name of Equipment

1.

Supersonic Wind Tunnel (1971)

2.

Subsonic Wind Tunnel (1971)

3.

Air Reservoir

4.

Reciprocating Air Compressor

5.

Honeywell Pressure Sensor 24PVEF6D

6.

Data Acquisition System

7.

Digital SLR Camera (Sony)

8.

1-Component Strain Gauge Balance

9.

Digital SLR Camera  (Canon)

10.

3-Component Strain Gauge Balance

11.

6-Component Strain Gauge Balance

12.

Unsteady Pressure Transducer

13.

Supersonic Wind Tunnel (2012)

14.

AC Variable Frequency Drive for AC Motor

15.

Pressure Scanner

16.

Inclinometer

17.

5-Component Strain Gauge Balance

18.

Signal Conditioner

19.

DC Power Supply

20.

6 ½ precision Multimeter

21.

Micro Welding Machine

22.

Air Compressor

23.

Single Channel Hot Wire Anemometer

24.

Free Jet Facility

25.

Anechoic Chamber

26.

Digital Storage Oscilloscope

27.

Schlieren Visualization System

Combustion Laboratory

1.

Flame Propagation and Stability Unit

2.

Differential Scanning Calorimeter

3.

Simultaneous Thermal Analyzer

4.

10 kVA UPS System, Battery, Rack

5.

DSC Sample Carrier System

6.

Digital Bomb Calorimeter

Liquid and Hybrid Propulsion Laboratory

1.

Unsteady Pressure Transducers

2.

PC based DATA Acquisition System

3.

Electro-Pneumatic Actuator  for LOX

4.

Electro-Pneumatic Actuator  for LH

5.

Control Valves Systems Assembly

6.

Software for High Speed Camera

7.

Differential Pressure Transducer & Sensor

8.

Liquid Propulsion Set up

9.

Turbine Flow Meter

10.

Upgraded Liquid Propulsion Thrust Stand

Propellant Technology Laboratory

1.

Stereo Microscope

2.

Fume Hood Operating System

3.

Sieve Shaker

4.

UV-Vis Spectrophotometer

5.

Sigma Blade Mixer

6.

2-Ton AC

7.

Bry Air Dryer

8.

Dehumidifier

9.

Environmental Chamber

10.

Infrared Pyrometer Impac SI 12

11.

Magnetic Stirrer-cum-Hot Plate

12.

Hot Air Oven

13.

Vacuum Oven

14.

Double Planetary Mixer

15.

High-Speed Dispenser

Solid Rocket Propulsion Laboratory

1.

Digital Viscometer  (LVDT)

2.

Shear Stress Analyser

3.

Data Acquisition and Analysis System for Solid Rocket Tests

4.

Electronic Analytical Semi Microbalance

5.

CAP 2000+ Viscometer

6.

Data Acquisition System 6036E

7.

Pressure Transducer and Electro- Pneumatic Valve, 0 - 50 Kg.

8.

i.  DAQ-9172-8 Slot USB

ii. NI 9229-4 Channel

iii. NI 9211-4 Channel 

9.

Thrust Chamber Assembly

10.

Digital Pressure Gauge

11.

5-Component Strain Gauge Balance

12.

Pulverizer

13.

Mechanical Stirrer

 

Departmental Workshop

1.

6 feet High-Precision All Geared Lathe Machine

 

CFD Laboratory

1.

10 Nos. of PCs

2.

Research License for Ansys CFD

 
Image Gallery of Facilities:
 
Aerodynamics
Low-Speed Wind Tunnel                                                          Supersonic Wind Tunnel
 
Supersonic Wind Tunnel                                                         Supersonic Wind Tunnel
 
 
Rocket Propulsion
Propellant Processing                                                             Bantam Mill
 
Bomb Calorimeter                                                                    DSC and TGA