Aerospace Research Centre - Anna University


Supersonic Tunnel
Subsoni Wind Tunnel
Speed = 320 kMPH
Test Section Size = 3X4X6 feet
Circular Cone Model Mounted in the test Section
Static Firing of Hybrid Rocket Motor(Nozzleless)& Thrust Measurement
Climatic Chamber - 990 liters Capacity
(WEISS Make Model WK111 – 1000)
Universal Testing Machine with Temperature
Cabinet (Instron make=336)

Dilato Meter
Laser Flash Apparatus



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