Thermal radiation of heterogeneous combustion products at the nozzle exit of the rocket microengine
Russian aeronautics ; 59 , 4
2016
Article (Journal)
English
Local classification TIB: | 770/7040/8000 | |
BKL: | 55.50 Luftfahrzeugtechnik |
Thermal radiation of heterogeneous combustion products at the nozzle exit of the rocket microengine
Springer Verlag | 2016
|Micro-Heat Engines, Gas Turbines, and Rocket Engines - The MIT Microengine Project -
British Library Conference Proceedings | 1997
|Use of Discontinuous Exit Flows to Reduce Rocket Nozzle Length
British Library Conference Proceedings | 1994
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