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International Journal of Aerospace Engineering
/
2021
/
Article
/
Tab 1
/
Research Article
Preliminary Research on a High Thrust-to-Weight Ratio of Double-Sided Composite Impeller Microturbine Engine
Table 1
Top-level parameters of a 230 N microturbojet engine [
11
].
Parameters
Value
Total pressure ratio
3.6
Mass flow (kg/s)
0.45
Turbine inlet total temperature (K)
1023
Rotating speed,
(r/min)
100000