Research Article
Study on Heat Exchange Structure Design and Propulsion Performance of Solar Thermal Thruster
Table 4
Parameters in simulation.
| | Parameters | Value |
| | Inlet pressure | | | Inlet temperature | 293 K | | Concentrator diameter | 0.1 m | | Light source power | 2000 W | | Nozzle throat diameter | 0.0013 m | | Nozzle outlet diameter | 0.0136 m | | Expansion angle of nozzle expansion section | 15° | | Expansion ratio of nozzle expansion section | 109.4430 | | Mass flow rate | | | Concentrator efficiency | 85% | | Nozzle efficiency | 95% |
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