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STAR
Cal STAR — firmware, DAQ server, and engine design
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Public Member Functions | |
| test_expansion_ratio_computed (self) | |
| test_moment_arm (self) | |
| test_r_specific (self) | |
| test_use_solved_plot_false_by_default (self) | |
| test_use_solved_plot_true_when_volume_set (self) | |
| test_effective_volume_chamber_auto_estimate (self) | |
| test_effective_volume_chamber_uses_explicit (self) | |
Definition at line 165 of file test_cold_gas_thruster.py.
| test_cold_gas_thruster.TestConfig.test_effective_volume_chamber_auto_estimate | ( | self | ) |
When volume_chamber=0, should estimate from A_chamber * chamber_length.
Definition at line 189 of file test_cold_gas_thruster.py.
References test_cold_gas_thruster._make_config().
| test_cold_gas_thruster.TestConfig.test_effective_volume_chamber_uses_explicit | ( | self | ) |
Definition at line 195 of file test_cold_gas_thruster.py.
References test_cold_gas_thruster._make_config().
| test_cold_gas_thruster.TestConfig.test_expansion_ratio_computed | ( | self | ) |
Definition at line 167 of file test_cold_gas_thruster.py.
References test_cold_gas_thruster._make_config().
| test_cold_gas_thruster.TestConfig.test_moment_arm | ( | self | ) |
Definition at line 172 of file test_cold_gas_thruster.py.
References test_cold_gas_thruster._make_config().
| test_cold_gas_thruster.TestConfig.test_r_specific | ( | self | ) |
Definition at line 176 of file test_cold_gas_thruster.py.
References test_cold_gas_thruster._make_config().
| test_cold_gas_thruster.TestConfig.test_use_solved_plot_false_by_default | ( | self | ) |
Definition at line 181 of file test_cold_gas_thruster.py.
References test_cold_gas_thruster._make_config().
| test_cold_gas_thruster.TestConfig.test_use_solved_plot_true_when_volume_set | ( | self | ) |
Definition at line 185 of file test_cold_gas_thruster.py.
References test_cold_gas_thruster._make_config().