Effect of various dimensions on performance of system was studied both theoretically and experimentally; theory employing nonviscous fluid mechanics is developed showing good agreement with experiments; results show that pumping fluid leaving nozzle can evacuate its own environment to minimum value of 0.025 atm.
Performance investigation of nonpumping rocket-ejector system for altitude simulation
NASA -- Tech Note
1959
33 pages
Report
English
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Methods for determining performance of ejector-diffuser systems used in rocket altitude simulation
Engineering Index Backfile | 1964
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