Multi-stage semiconductor thermoelectric power generation and cooling integrated system for hypersonic flight vehicle
Multi-stage semiconductor thermoelectric power generation and cooling integrated system for hypersonic flight vehicle
- CN 106,533,263 A
- Filed: 12/29/2016
- Published: 03/22/2017
- Est. Priority Date: 12/29/2016
- Status: Active Application
- EN CH
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- Pin
