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| Micro-Wireless Instrumentation System (Micro-WIS) |
| DTO HTD 1403 |
| Overview |
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This HTD will demonstrate the operational utility and functionality of Micro-WIS on orbit, initially in the crew cabin of the orbiter and then in the International Space Station. The Micro-WIS sensor/transmitter will provide important real-time temperature measurements. The Micro-WIS sensor/recorder will provide recorded temperature readings for postflight evaluation. |
| History/Background |
| This is the fifth flight of HTD 1403. |
Editorial/Technical Comments: ShuttlePresskit
