Dear all,

We have MEMS sensors and actuators on a missile nose-cone for testing. Can
anyone please help us in determining the temperature range for supersonic
testing around Mach 1 for these sensors in a wind tunnel? Or if anyone
knows what temperature range will  be the missile model subject to at Mach
1, we can work out the rest.

Thanks,
Mehul Patel
440-449-5785
Mechanical Engg.
CWRU.