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  • 1
    Publication Date: 2019-06-27
    Description: An evaluation of a scale model of a low pressure rocket engine which is used for secondary injection studies was conducted. Specific objectives of the evaluation were to: (1) assess the test conditions required for full scale simulations; (2) recommend fluids to be used for both primary and secondary flows; and (3) recommend possible modifications to be made to the scale model and its test facility to achieve the highest possible degree of simulation. A discussion of the theoretical and empirical scaling laws which must be observed to apply scale model test data to full scale systems is included. A technique by which the side forces due to secondary injection can be analytically estimated is presented.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-CR-124176 , HREC-8899-2 , LMSC/HREC-D306359
    Format: application/pdf
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