University of South Alabama Mobile, Alabama FRR. Team Members Tim Morgan Alex Scruggs David Shaw Andy Mosley Joseph McCreary Nick Hall. Launch Vehicle General Dimensions. Length = 118.3 “ Diameter = 4” Mass = 13.5 oz. Launch Vehicle Components. Nose Cone Plastic 3.9 “ Diameter
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Purpose: Collect Pressure, Temperature and Humidity Data
Implementation: Use G-Whiz HCX Flight Computer to record data from Vaisala HMP 50 Temperature/Humidity Probe
1. Brown +VDC 7 to 28 VDC
2. White +0…. 1/2.5/5 V 0 to 100 %
3. Blue -VDC
4. Black 0... 1/2.5/5 V -40 to +60 °C